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Books

• Qin N, Periaux J & Bugeda G (2019) Advances in Effective Flow Separation Control for Aircraft Drag Reduction Modeling, Simulations and Experimentations. Springer.
• beck S, blakey S, chin S, Nicolleau FCGA, qin N, Brown M & Wilson C (2006) The little book of thermofluids. ºù«Ӱҵ: University of ºù«Ӱҵ Dept.of Mechanical & Process Engineering.

Journal articles

• Chen H, Wang Z, Tian L, Liu J, Qin N & Zhao N (2025) . Physics of Fluids, 37(1).
• Bidar O, Anderson SR & Qin N (2024) . Physics of Fluids, 36(1).
• Xue C, Deng F, Wang H & Qin N (2023) . International Journal of Aerospace Engineering, 2023.
• Cuciumita C, Qin N & Shahpar S (2023) . Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy.
• Wang H, Deng F, Liu X & Qin N (2022) . Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 43(11).
• Zhang S, Deng F, Qin N & Liu X (2022) . Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 43(11).
• Yi J, Deng F, Qin N & Liu X (2022) . Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 43(11).
• Zhang S, Deng F & Qin N (2022) . Aerospace, 9(11).
• Li Y & Qin N (2022) . Applied Sciences, 12(20).
• Deng F, Wang H, Xue C & Qin N (2022) . Aerospace Science and Technology, 107935-107935.
• Xie F, Pérez-Muñoz JD, Qin N & Ricco P (2022) . Journal of Fluid Mechanics, 941.
• Li Y & Qin N (2021) . Journal of Fluids and Structures, 107, 103407.
• Li Y & Qin N (2021) . Aerospace Science and Technology, 117.
• Deng F & Qin N (2021) . AIAA Journal.
• Zhu M & Qin N (2021) . AIAA Journal.
• Chen Z, Xiao T, Wang Y & Qin N (2021) . Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering.
• Vivarelli G, Qin N, Shahpar S & Radford D (2021) . Computers & Fluids, 104929-104929.
• Hollom J & Qin N (2021) . The Aeronautical Journal, 125(1284), 365-388.
• John A, Bower J, Qin N, Shahpar S & Smith A (2020) . The Aeronautical Journal, 124(1282), 1913-1944.
• Vivarelli G, Qin N, Shahpar S & Radford D (2020) . International Journal for Numerical Methods in Fluids.
• Apetrei RM, Ciobaca V, Curiel-Sosa JL & Qin N (2020) . Advances in Aerodynamics, 2(1).
• Li Y & Qin N (2020) . Journal of Aircraft, 57(3), 408-417.
• Li Y & Qin N (2019) . Aerospace Science and Technology.
• Liu S, Wang Y, Qin N & Zhao N (2019) . AIAA Journal.
• Ahmed MYM & Qin N (2019) . Progress in Aerospace Sciences.
• John A, Qin N & Shahpar S (2019) . Journal of Turbomachinery, 141(8).
• Zhu M, Li Y, Qin N, Huang Y, Deng F, Wang Y & Zhao N (2019) . AIAA Journal, 57(6), 2408-2420.
• Apetrei R, Curiel-Sosa JL & Qin N (2018) . Journal of Aircraft.
• Wang Y, Qin N & Zhao N (2018) . Chinese Journal of Aeronautics, 31(11), 2093-2103.
• Badcock KJ, Barakos GN, Cummings RM, Platzer M, Qin N, Sieverding CH & Wendt J (2018) . Progress in Aerospace Sciences, 101, 1-12.
• Deng F & Qin N (2018) . Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 233(7), 2344-2359.
• John A, Qin N & Shahpar S (2018) . Journal of Turbomachinery, 140(6).
• Deng F, Xie F, Qin N, Huang W, Wang L & Chu H (2018) . Aerospace Science and Technology, 76, 361-373.
• Mura GL, Hinchliffe BL, Qin N & Brezillon J (2018) . AIAA Journal, 56(4), 1541-1553.
• Xiao T, Qin N, Lu Z, Sun X, Tong M & Wang Z (2017) . Aerospace Science and Technology, 66, 28-43.
• Wang Y, Qin N & Zhao N (2017) . Communications in Computational Physics, 21(5), 1282-1309.
• Chen H & Qin N (2017) . Renewable Energy, 105, 419-435.
• Deng F, Jiao Z, Liang B, Xie F & Qin N (2017) . Journal of Spacecraft and Rockets, 54(6), 1185-1195.
• Mura GL, Hinchliffe BL, Qin N & Brezillon J (2017) . AIAA Journal, 55(4), 1140-1151.
• John A, Shahpar S & Qin N (2017) . Journal of Turbomachinery, 139(8).
• Hinchliffe B & Qin N (2016) . AIAA Journal, 55(3), 818-831.
• Xiao T, Qin N, Luo D & Deng S (2016) . AIAA Journal, 54(8), 2392-2406.
• Wang W, Nicolleau FCGA & Qin N (2016) . Fluid Dynamics Research, 48(2).
• Zeng M, Xu D, Liu J & Qin N (2016) . Journal of Thermophysics and Heat Transfer, 30(1), 12-24.
• Wang Y, Qin N & Zhao N (2015) . Journal of Computational Physics, 294, 149-172.
• Qin N (2015) . The Aeronautical Journal, 119(1214), 560-560.
• Liu S & Qin N (2015) . Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 229(2), 280-289.
• Wang H, Sun M, Yang Y & Qin N (2015) . International Journal of Hydrogen Energy, 40(33), 10658-10661.
• Harris MJ & Qin N (2015) . AIAA Journal, 53(1), 246-259.
• Harris MJ & Qin N (2014) . Computers & Fluids, 102, 1-14.
• Wang H, Wang Z, Sun M & Qin N (2014) . Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 228(4), 530-541.
• Zhu F & Qin N (2014) . AIAA Journal, 52(1), 17-25.
• Wang W, Siouris S & Qin N (2014) . Aircraft Engineering and Aerospace Technology, 86(3), 179-187.
• Wang Y, Qin N, Carnie G & Shahpar S (2013) . Journal of Computational Physics, 255(0), 130-148.
• McIntosh SC & Qin N (2013) . AERONAUTICAL JOURNAL, 117(1196), 1037-1051.
• Deng F, Qin N, Liu X, Yu X & Zhao N (2013) . Science China Technological Sciences, 56(10), 2385-2390.
• Deng F, Qin N & Wu Y (2013) Shock control bump optimization for drag reduction using parallel efficient global optimization algorithm. Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics, 45(4), 485-490.
• Yang Y, Ouyang S, Liu X & Qin N (2013) Aerodynamic optimization of transonic wing using discrete adjoint operator. Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics, 45(3), 347-352.
• Lu Q, Chen J, Qin N & Wang X (2013) Design of tip airfoil of wind turbine based on hybrid parameterization modification theory. Taiyangneng Xuebao/Acta Energiae Solaris Sinica, 34(4), 555-561.
• García Naranjo A, Cowling I, Green JA & Qin N (2013) Aerodynamic performance, benefits of utilising camber morphing wings for unmanned air vehicles. Aeronautical Journal, 117(1189), 329-340.
• Naranjo AG, Cowling I, Green JA & Qin N (2013) . AERONAUTICAL JOURNAL, 117(1189), 315-327.
• Qin N, Carnie G, Wang Y & Shahpar S (2013) . Journal of Turbomachinery, 136(3).
• Chen ZJ & Qin N (2013) . JOURNAL OF AIRCRAFT, 50(3), 952-964.
• Chen ZJ, Qin N & Nowakowski AF (2013) . Journal of Aircraft, 50(1), 152-163.
• Wang H, Wang Z, Sun M & Qin N (2013) . Science China Technological Sciences, 1-14.
• Wu WH, Fan ZL, Chen DH, Qin N & Meng DH (2012) Adjoint based on high precise aerodynamic shape optimization for transonic civil aircraft. Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 30(6).
• Danao L, Qin N & Howell RJ (2012) . Proceedings of the Institution of Mechanical Engineers, Part A, Journal of Power and Energy.
• WU W, CHEN D, QIN N, PENG XIN & TANG X (2012) . International Journal of Modern Physics: Conference Series, 19, 396-405.
• Wang W & Qin N (2012) . Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 117, 379-388.
• Deng F, Qin N & Wu Y (2012) Training algorithms for EGO method and applications. Jisuan Wuli/Chinese Journal of Computational Physics, 29(3), 326-332.
• Durrani N & Qin N (2012) . Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 117, 257-266.
• Ahmed MYM & Qin N (2012) . AIAA Journal, 50(4), 797-810.
• Qin N, Howell R, Durrani N, Hamada K & Smith T (2011) . Wind Engineering, 35(4), 511-527.
• Ahmed MYM & Qin N (2011) Numerical investigation of aeroheating characteristics of spiked blunt bodies at Mach six flight conditions. AERONAUT J, 115(1168), 377-386.
• Lee DS, Periaux J, Onate E, Gonzalez LF & Qin N (2011) . JOURNAL OF AIRCRAFT, 48(3), 1084-1094.
• Lee DS, Periaux J, Srinivas K, Gonzalez LF, Qin N & Onate E (2011) . Computational Fluid Dynamics 2010 - Proceedings of the 6th International Conference on Computational Fluid Dynamics, ICCFD 2010, 253-259.
• Ahmed MYM & Qin N (2011) . Progress in Aerospace Sciences, 47(6), 425-449.
• Zheng HW, Shu C, Chew YT & Qin N (2011) . International Journal for Numerical Methods in Fluids, 67(5), 616-637.
• Ahmed MYM & Qin N (2011) Recent advances in the aerothermodynamics of spiked hypersonic vehicles. Progress in Aerospace Sciences.
• Durrani N & Qin N (2011) . Journal of Aircraft, 48(1), 193-202.
• Zheng HW, Qin N, Nicolleau FCGA & Shu C (2011) . Communications in Computational Physics, 9(1), 68-88.
• Elarbi EM & Qin N (2010) Effects of pitching rotation on aerodynamics of tandem flapping wing sections of a hovering dragonfly. AERONAUT J, 114(1161), 699-710.
• De Feo D, Qin N & Birch TJ (2010) . ADV APPL MATH MECH, 2(4), 399-429.
• Ahmed MYM & Qin N (2010) . AEROSP SCI TECHNOL, 14(5), 364-376.
• Howell R, Qin N, Edwards J & Durrani N (2010) . RENEW ENERG, 35(2), 412-422.
• Ahmed MYM & Qin N (2010) . J SPACECRAFT ROCKETS, 47(1), 62-80.
• Pang XP, Qin N, Dwyer-Joyce RS, Chen J & Wang JX (2010) . TRIBOL T, 53(1), 117-126.
• Shan YY, Shu C & Qin N (2009) . ADV APPL MATH MECH, 1(5), 615-638.
• Wong WS, Qin N, Sellars N, Holden H & Babinsky H (2008) . AEROSP SCI TECHNOL, 12(6), 436-447.
• Qin N & Xia H (2008) . P I MECH ENG I-J SYS, 222(I5), 373-380.
• Qin N, Wong WS & Le Moigne A (2008) . P I MECH ENG G-J AER, 222(G5), 619-629.
• Boller C, Kuo CM & Qin N (2008) Biologically Inspired Shape Changing Aerodynamic Profiles and their Effect on Flight Performance of Future Aircraft. Advances in Science and Technology, 56, 534-544.
• Liu X, Li Q, Chai J & Qin N (2008) New dynamic grid algrithm and its application. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 29(4), 817-822.
• Zhong B, Shaw S & Qin N (2007) . INT J NUMER METH FL, 55(6), 509-536.
• Shu C, Shan YY & Qin N (2007) . INT J NUMER METH FL, 55(4), 367-386.
• Qin N & Hodgkinson JM (2007) Promoting scientific and technical communication in aerospace engineering with China. P I MECH ENG G-J AER, 221(G2), I-I.
• Wong WS, Le Moigne A & Qin N (2007) Parallel adjoint-based optimisation of a blended wing body aircraft with shock control bumps. AERONAUT J, 111(1117), 165-174.
• Spence GT, Le Moigne A, Allerton DJ & Qin N (2007) . J AIRCRAFT, 44(2), 467-475.
• Vavalle A & Qin N (2007) . J AIRCRAFT, 44(2), 365-376.
• Qin N & Hodgkinson JM (2007) . Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 221(2), i-i.
• Siouris S & Qin N (2007) . P I MECH ENG G-J AER, 221(G1), 47-55.
• Le Moigne A & Qin N (2006) Aerofoil profile and sweep optimisation for a blended wing-body aircraft using a discrete adjoint method. AERONAUT J, 110(1111), 589-604.
• Qin N & Liu XQ (2006) . INT J NUMER METH ENG, 67(6), 894-894.
• Qin N & Liu XQ (2006) . INT J NUMER METH ENG, 67(6), 787-814.
• Liu XQ, Qin N & Xia H (2006) . J COMPUT PHYS, 211(2), 405-423.
• Qin N, Liu X & Xia H (2005) An efficient moving grid algorithm for large deformation. MODERN PHYSICS LETTERS B, 19(28-29), 1499-1502.
• Xia H & Qin N (2005) Detached-Eddy Simulation for synthetic jets with moving boundaries. MODERN PHYSICS LETTERS B, 19(28-29), 1429-1434.
• Anwar-ul-Haque , Qin N & Umar F (2005) . The Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF), 2005(0), 661-666.
• Tadjouddine M, Forth SA & Qin N (2005) . INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 47(10-11), 1315-1321.
• Qin N, Vavalle A & Le Moigne A (2005) Spanwise lift distribution for blended wing body aircraft. J AIRCRAFT, 42(2), 356-365.
• Qin N, Vavalle A, Le Moigne A, Laban M, Hackett K & Weinerfelt P (2004) . PROG AEROSP SCI, 40(6), 321-343.
• Le Moigne A & Qin N (2004) Variable-fidelity aerodynamic optimization for turbulent flows using a discrete adjoint formulation. AIAA J, 42(7), 1281-1292.
• Qin N, Zhu Y & Shaw ST (2004) Numerical study of active shock control for transonic aerodynamics. INT J NUMER METHOD H, 14(4), 444-466.
• Prince SA & Qin N (2002) Mechanism of windward vortex shocks about supersonic slender bodies. AERONAUT J, 106(1063), 507-519.
• Qin N & Chong Y (2002) Monotone integrated large eddy simulations for supersonic boundary layer flows. Computational Fluid Dynamics Journal, 10(4), 548-552.
• Zhong B & Qin N (2001) Non-inertial multiblock Navier-Stokes calculation for hovering rotor flowfields using relative velocity approach. AERONAUT J, 105(1049), 379-389.
• Richardson G & Qin N (2001) An eddy-viscosity limited algebraic stress model for shook-boundary-layer interaction. AERONAUT J, 105(1045), 105-118.
• Shaw ST & Qin N (2001) Study of the aerodynamics of in-plane motion. P I MECH ENG G-J AER, 215(G2), 89-104.
• Shaw ST & Qin N (2000) Calculation of compressible indicial response. AERONAUT J, 104(1042), 665-673.
• Qin N, Ludlow DK & Shaw ST (2000) A matrix-free preconditioned Newton/GMRES method for unsteady Navier-Stokes solutions. INT J NUMER METH FL, 33(2), 223-248.
• Kontis K, Qin N, Stollery JL & Edwards JA (2000) Hypersonic performance of a lifting elliptic cone with and without strakes. JOURNAL OF SPACECRAFT AND ROCKETS, 37(1), 21-27.
• Qin N & Zhu Y (1999) Grid adaption for shock/turbulent boundary-layer interaction. AIAA JOURNAL, 37(9), 1129-1131.
• Qin N & Redlich A (1999) Massively separated flows due to transverse sonic jet in laminar hypersonic stream. SHOCK WAVES, 9(2), 87-93.
• Shaw ST & Qin N (1999) Unsteady flow around helicopter rotor blade sections in forward flight. AERONAUT J, 103(1019), 35-44.
• Ludlow DK & Qin N (1998) Computational prediction of pitch damping for supersonic blunt cones. JOURNAL OF SPACECRAFT AND ROCKETS, 35(6), 849-851.
• Qin N, Zhu Y & Poll DIA (1998) Surface suction on aerofoil aerodynamic characteristics at transonic speeds. P I MECH ENG G-J AER, 212(G5), 339-351.
• Qin N, Ludlow DK, Shaw ST, Edwards JA & Dupuis A (1997) Calculation of pitch damping for a flared projectile. JOURNAL OF SPACECRAFT AND ROCKETS, 34(4), 566-568.
• Qin N (1996) Incipient separation boundary: Confirmation of an empirical criterion by Navier-Stokes solutions. AERONAUT J, 100(999), 381-384.
• Qin N & Foster GW (1996) Computational study of supersonic lateral jet flow interactions. J SPACECRAFT ROCKETS, 33(5), 651-656.
• XU X, QIN N & RICHARDS BE (1992) ALPHA-GMRES - A NEW PARALLELIZABLE ITERATIVE SOLVER FOR LARGE SPARSE NONSYMMETRICAL LINEAR-SYSTEMS ARISING FROM CFD. INT J NUMER METH FL, 15(5), 613-623.
• Qin N, Xu X & Richards BE (1992) Newton-like methods for Navier-Stokes solution.
• Qin N, Xu X & Richards BE (1992) . Computing Systems in Engineering, 3(1-4), 429-435.
• Qin N, Xu X & Richards BE (1992) Newton-like methods for Navier-Stokes solution.
• QIN N, SCRIBA KW & RICHARDS BE (1991) SHOCK-SHOCK, SHOCK-VORTEX INTERACTION AND AERODYNAMIC HEATING IN HYPERSONIC CORNER FLOW. AERONAUT J, 95(945), 152-160.
• Qin N & Richards BE (1990) , 474-483.
• Qin N & Richards BE (1988) Sparse quasi-Newton method for high resolution schemes. Notes on Numerical Fluid Mechanics, 20, 310-317.
• Qin N (1984) An Inverse method for boundary separated flows. Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 4(4), 12-21.
• Zhi H, Xiao T, Qin N, Deng S & Lu Z () . AIAA Journal, 1-19.
• Chen Z, Wei X, Xiao T & Qin N () . Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering.
• Deng S, Wang Y & Qin N () . AIAA Journal, 1-16.
• Deng F, Zhang S & Qin N () . Aerospace, 10(6), 537-537.
• Stannard A & Qin N () . AIAA Journal, 1-14.
• Vincekovic L, John A, Qin N & Shahpar S () . Journal of Turbomachinery, 1-14.
• Deng F, Xue C & Qin N () . AIAA Journal, 1-14.
• Wang Y, Liu S, Qin N & Zhao N () . Journal of the Chinese Institute of Engineers, 1-9.
• Deng F & Qin N () . Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 095441002110324-095441002110324.
• Qin N & Richards BE () , 453-454.
• Qin N & Richards BE () , 528-532.
• Fan Z, Yu X, Qin N & Zhu M () . Journal of Aircraft, 1-8.

Chapters

• Bidar O, Anderson SR & Qin N (2025) , Proceedings of the Cambridge Unsteady Flow Symposium 2024 (pp. 121-133). Springer Nature Switzerland
• Li Y & Qin N (2022) , Advances in Computational Methods and Technologies in Aeronautics and Industry (pp. 105-116). Springer International Publishing
• Gonzalez P & Qin N (2020) , Advances in Effective Flow Separation Control for Aircraft Drag Reduction (pp. 93-112). Springer International Publishing
• Bonnet J-P & Qin N (2020) , Advances in Effective Flow Separation Control for Aircraft Drag Reduction (pp. 1-26). Springer International Publishing
• Gonzalez P, Qin N & Ming X (2020) , Advances in Effective Flow Separation Control for Aircraft Drag Reduction (pp. 255-264). Springer International Publishing
• Siouris S, Wang W & Qin N (2020) , Advances in Effective Flow Separation Control for Aircraft Drag Reduction (pp. 327-341). Springer International Publishing
• Siouris S & Qin N (2020) , Advances in Effective Flow Separation Control for Aircraft Drag Reduction (pp. 131-143). Springer International Publishing
• Bugeda G, Périaux J, Qin N & Pons-Prats J (2020) , Advances in Effective Flow Separation Control for Aircraft Drag Reduction (pp. 27-53). Springer International Publishing
• Lo KH, Zare-Behtash H, Kontis K & Qin N (2015) , 29th International Symposium on Shock Waves 1 (pp. 441-446). Springer International Publishing
• Zheng HW, Shu C, Chew YT & Qin N (2012) , ERCOFTAC Series (pp. 103-117). Springer Netherlands
• Zheng HW, Nicolleau FCGA & Qin N (2011) In Nicolleau FCGA, Cambon C, Redondo J-M, Vassilicos JC, Reeks M & Nowakowski AF (Ed.), New approaches in modelling multiphase flows and dispersion in turbulence, fractal methods and synthetic turbulence (pp. 9-21). Springer Netherlands
• Boller C, Kuo CM & Qin N (2007) In Davis LP, Henderson BK & McMickell MB (Ed.), SPIE Smart Structures and Materials & Nondestructive Evaluation and Health Monitoring, 18 - 22 March 2007, San Diego, California USA (pp. K5270-K5270).
• Qin N (2006) From flying wings to blended wing body aircraft,, McGraw-Hill Yearbook of Science and Technology 2006 McGraw-Hill Professional; Revised edition edition (1 Jan. 2006)
• (2001) Springer US

Conference proceedings papers

• Bidar O, He P, Anderson S & Qin N (2024) . AIAA SCITECH 2024 Forum
• Bidar O, Anderson S & Qin N (2024) . AIAA SCITECH 2024 Forum
• Liu Y, Xiao J, Benai-Dara NA, Chen Z & Qin N (2024) Experimental and Numerical Investigation on Aerodynamic Performance of a Mars Rotor System. ICAS Proceedings
• Cuciumita C, Qin N, Shahpar S & Namgoong H (2023) . Volume 13D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Radial Turbomachinery Aerodynamics; Unsteady Flows in Turbomachinery, 26 June 2023 - 30 June 2023.
• Vincekovic L, Qin N & Shahpar S (2021) . AIAA AVIATION 2021 FORUM
• Cuciumita C, John A, Qin N & Shahpar S (2021) . Volume 2D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Radial Turbomachinery Aerodynamics; Unsteady Flows in Turbomachinery, 7 June 2021 - 11 June 2021.
• Cuciumita C, Qin N, Stanley F & Shahpar S (2021) . Volume 9B: Structures and Dynamics — Fatigue, Fracture, and Life Prediction; Probabilistic Methods; Rotordynamics; Structural Mechanics and Vibration, 7 June 2021 - 11 June 2021.
• John A, Vivarelli G, Qin N & Shahpar S (2020) . Volume 2C: Turbomachinery, 21 September 2020 - 25 September 2020.
• John A, Qin N & Shahpar S (2020) . Volume 2D: Turbomachinery, 21 September 2020 - 25 September 2020.
• Vincekovic L, John A, Qin N & Shahpar S (2020) . Volume 2B: Turbomachinery, 21 September 2020 - 25 September 2020.
• John A, Qin N & Shahpar S (2018) . Volume 2A: Turbomachinery, 11 June 2018 - 15 June 2018.
• Vivarelli G, Qin N, Shahpar S & Radford D (2018) . Volume 2C: Turbomachinery, 11 June 2018 - 15 June 2018.
• Apetrei R, Curiel-Sosa JL & Qin N (2018) Prediction of Unsteady Transonic Buffeting using the SU2 Open-Source Code. Proceedings of the 7th European Conference on Computational Fluid Dynamics (ECFD 7). Glasgow, 11 June 2018 - 15 June 2018.
• Vivarelli G, Qin N, Shahpar S & Radford D (2018) . Proceedings of the ASME Turbo Expo, Vol. 2C-2018
• Hollom J & Qin N (2018) . 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
• Deng F & Qin N (2018) An efficient multiobjective global optimization algorithm for expensive aerodynamic shape optimizations. 10th International Conference on Computational Fluid Dynamics, ICCFD 2018 - Proceedings
• John A, Qin N & Shahpar S (2017) . Volume 2A: Turbomachinery, 26 June 2017 - 30 June 2017.
• Hollom J & Qin N (2017) . 18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
• John A, Qin N & Shahpar S (2017) Understanding fan blade tip aerodynamics. 12th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2017
• John A, Qin N & Shahpar S (2017) . Proceedings of the ASME Turbo Expo, Vol. 2A-2017
• Mura GL, Hinchliffe BL, Qin N & Brezillon J (2017) . 55th AIAA Aerospace Sciences Meeting
• John A, Qin N & Shahpar S (2017) Understanding fan blade tip aerodynamics. 12th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2017
• Vivarelli G, Qin N & Shahpar S (2017) . 55th AIAA Aerospace Sciences Meeting
• Mura GL & Qin N (2017) . 55th AIAA Aerospace Sciences Meeting
• John A, Shahpar S & Qin N (2017) . 12th European Conference on Turbomachinery Fluid Dynamics and hermodynamics, 3 April 2017 - 7 April 2017.
• John A, Qin N & Shahpar S (2017) Understanding fan blade tip aerodynamics. European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC
• Qin N & Pratt T (2016) Vortex Generators for Increased Maximum Lift and Enhanced High-α Stability of a Zimmerman-Wing MAV at Low Reynolds Number. 2016 Applied Aerodynamics Conference
• Qin N, mura G & hinchliffe B (2016) Robust Delaunay Graph Based Mesh Movement for Adjoint Mesh Sensitivity. 2016 Applied Aerodynamics Conference
• John A, Shahpar S & Qin N (2016) . Volume 2A: Turbomachinery, 13 June 2016 - 17 June 2016.
• Mura GL, Hinchliffe BL, Qin N & Brezillon J (2016) . 54th AIAA Aerospace Sciences Meeting
• Qin N, Xiao T, Luo D & Deng S (2016) . 54th AIAA Aerospace Sciences Meeting, 4 January 2016 - 8 January 2016.
• Hinchliffe BL & Qin N (2016) . 54th AIAA Aerospace Sciences Meeting
• McCartney B, Prince S & Qin N (2016) The effect of leading edge rounding on a caret waverider configuration at Mach 8.2. 30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016
• WANG Y, QIN N & ZHAO N (2016) . International Journal of Modern Physics: Conference Series, Vol. 42 (pp 1660166-1660166)
• Lu Z, Xiao T, Qin N, Sun X, Tong M & Wang Z (2016) Investigation of pitching angle on pressure load for ditching of helicopter using SPH method. 46th AIAA Fluid Dynamics Conference
• Chen JZ & Qin N (2015) . 53rd AIAA Aerospace Sciences Meeting
• Zhu F & Qin N (2015) . 53rd AIAA Aerospace Sciences Meeting
• Yibin W, Ning Q & Xueqiang L (2015) . Procedia Engineering, Vol. 99 (pp 507-514)
• Qin N & Yu H (2014) Effects of Gurney Flap and Shock Bump on Supercritical and NLF Transonic Aerofoil. Royal Aeronautical Society Applied Aerodynamics Conference 2014. London, UK, 22 July 2014 - 24 July 2014.
• Qin N & Zhu F (2014) Further Development of CST Geometric Parameterisation Method forAdjoint Aerodynamic Optimisation. ADVANCED AERO CONCEPTS, DESIGN AND OPERATIONS, APPLIED AERODYNAMICS CONFERENCE 2014. London, 22 July 2014 - 24 July 2014.
• Qin N & Hinchliffe B (2014) Robust Design of 3D Shock Control Bumps on a Transonic Wing. ADVANCED AERO CONCEPTS, DESIGN AND OPERATIONS, APPLIED AERODYNAMICS CONFERENCE 2014. London, 22 July 2014 - 24 July 2014.
• Qin N & Harris M (2013) Using the Medial Axis to Represent Complex Flow Structures for Flow Feature-Aligned Mesh Generation. AIAA Paper 2013-0150. Grapevine, Texas, USA, 7 January 2013 - 13 January 2013.
• Qin N (2012) Multi-Objective Aerothermodynamic Design of Hypersonic Spikes and Forebodies. Proceedings of International Symposium on Hypersonic Aerothermodynamics – Recent Advances. Bangalore, India, 9 December 2012 - 13 December 2012.
• Qin N (2012) Simulation of aerodynamic flow control. The 2nd International Conference on Scientific Computing in Aerodynamics. Beijing, China, 18 October 2012 - 20 October 2012.
• Qin N (2012) Hybrid RANS/LES Simulation of Flow Control. Proceedings of the 9th Asian Computational Fluid Dynamics Conference. Nanjing, China, 11 October 2012 - 13 October 2012.
• Deng F, Liu X, Yu XQ & Qin N (2012) Shock Control Bump Optimization For a Low Sweep Supercritical Wing And Its Impact On Fuel Reduction. Proceedings of the 9th Asian Computational Fluid Dynamics Conference. Nanjing, China, 11 October 2012 - 13 October 2012.
• Qin N & Wang Y (2012) A New Method For Linking Two Dissimilar Structured Meshe. Proceedings of the 9th Asian Computational Fluid Dynamics Conference. Nanjing, China, 11 October 2012 - 13 October 2012.
• Zhu F & Qin N (2012) Development of CST Geometric Parameterisation Method for an Entire Transport Aircraft. RAeS Applied Aerodynamic Conference: Modelling and Simulation in the Aerodynamic Design Process, 17 July 2012 - 19 July 2012.
• Chen ZJ & Qin N (2012) Propeller Effects on Low Reynolds Number Aerodynamics. RAeS Applied Aerodynamic Conference: Modelling and Simulation in the Aerodynamic Design Process, 17 July 2012 - 19 July 2012.
• Ahmed M & Qin N (2012) Investigation of the flow asymmetry around axi-symmetric spiked blunt bodies at hypersonic speeds. RAeS Applied Aerodynamic Conference: Modelling and Simulation in the Aerodynamic Design Process, 17 July 2012 - 19 July 2012.
• Qin N (2012) (pp 45-53)
• Deng F, McIntosh SC & Qin N (2012) (pp 251-256)
• Ahmed MYM & Qin N (2012) (pp 727-733)
• Wang Y, Qin N & Liu X (2012) (pp 165-171)
• Qin N, Wang Y, Carnie G & Shahpar S (2011) . Proceedings of the 20th International Meshing Roundtable, IMR 2011 (pp 587-599)
• Carnie G, Wang Y, Qin N & Shahpar S (2011) . Proceedings of the ASME Turbo Expo, Vol. 7(GT2011-45483) (pp 1163-1174). Vancouver, Canada, 6 June 2011 - 10 June 2011.
• McIntosh S & Qin N (2011) Boundary Layer Effects on Shock Bump Performance. RAeS Aerodynamics Conference 2010, Applied Aerodynamics: Capabilities and Future Requirements. Bristol, UK, 27 July 2011 - 28 July 2011.
• Lee D, Periaux J, Gonzalez L, Onate E & Qin N (2011) . 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
• Durrani N & Qin N (2011) . 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
• Durrani N, Qin N, Hameed H & Khushnood S (2011) . 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
• Durrani N, Zaheer S & Qin N (2011) . 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
• Lu Q, Chen J, Cheng J, Qin N & Danao LAM (2011) . ICMREE2011 - Proceedings 2011 International Conference on Materials for Renewable Energy and Environment, Vol. 1 (pp 596-600)
• De Feo DM, Qin N & Birch TJ (2010) A MUSCL and WENO - PNS approach for vortex dominated flowfields. AIAA Paper 2010-503. Orlando, Florida, USA, 4 January 2010 - 7 January 2010.
• Qin N & Ahmed M (2010) Drag Reduction Using Aerodisks for Hypersonic Hemispherical Bodies. CEAS 2009 Air and Space Conference. Manchester, UK, 26 October 2009 - 29 October 2009.
• Coppin J & Qin N (2010) Alleviating UAV Pitch Divergence at High Lift Condition. RAeS Aerodynamics Conference 2010, Applied Aerodynamics: Capabilities and Future Requirements. London, 27 July 2010 - 28 July 2010.
• Elarbi E & Qin N (2010) Numerical Simulations of Plunging NACA0012 Wing for MAV Propulsion Systems. International Micro Air Vehicle Conference and Flight Competition, IMAV 2010. Braunschweig, Germany, 6 July 2010 - 9 July 2010.
• Durrani N & Qin N (2010) Detached-Eddy Simulation of Weapon Bay at Transonic Speed. IBCAST 2010 : The 7th International Bhurban Conference on Applied Sciences & Technology. Islamabad, Pakistan, 11 January 2010 - 14 January 2010.
• Ahmed MYM & Qin N (2010) . 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition(AIAA-2010-1318). Orlando, Florida, USA, 4 January 2010 - 7 January 2010.
• Zheng HW, Qin N & Shu C (2010) Three dimensional adaptive method for compressible multi-fluids flows. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition(AIAA-2010-812). Orlando, Florida, USA, 4 January 2010 - 8 January 2010.
• Chen ZJ, Nowakowski AF & Qin N (2010) Flow separation on cambered plate wing MAVs with various aspect ratios. RAeS Conference on Applied Aerodynamics: Capabilities and Future Requirements
• Zheng HW, Nicolleau FCGA & Qin N (2010) . Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 111 (pp 157-165)
• Elarbi E & Qin N (2009) Flapping Wing Simulation and Kinematics Analysis Based on Dragonfly Wing Section in Hover. CEAS 2009 Air and Space Conference. Manchester, UK, 26 October 2009 - 29 October 2009.
• Mohamed M & Qin N (2009) Control of NACA0015 Aerofoil Stall using Synthetic Jet Actuators. CEAS 2009 Air and Space Conference. Manchester, UK, 26 October 2009 - 29 October 2009.
• DeFeo D & Qin N (2009) Vortex Capturing Using PNS-WENO Schemes. CEAS 2009 Air and Space Conference. Manchester, UK, 26 October 2009 - 29 October 2009.
• Qin N (2009) Mesh movement, adaptation and feature alignment. Modern Trends in Computational Aerodynamics (Invited). Birmingham, UK, 16 September 2009 - 16 September 2009.
• Ahmed M & Qin N (2009) Comparison of Response Surface and Kriging Surrogates in Aerodynamic Design Optimization of Hypersonic Spiked Blunt Bodies. Aerospace Science and Technology Conference. Egypt, 1 May 2009 - 5 May 2009.
• Qin N, Carnie G, LeMoigne A, Liu X & Shahpar S (2009) Buffer layer method for linking two non-matching multi-block structured grids. 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition(AIAA-2009-1361). Orlando, Florida, USA, 5 January 2009 - 8 January 2009.
• Zheng HW, Nicolleau FCGA & Qin N (2009) . ADVANCES IN TURBULENCE XII - PROCEEDINGS OF THE 12TH EUROMECH EUROPEAN TURBULENCE CONFERENCE, Vol. 132 (pp 947-948)
• Boller C, Kuo CM & Qin N (2009) Biologically Inspired Shape Changing Aerodynamic Profiles and their Effect on Flight Performance of Future Aircraft. EMBODING INTELLIGENCE IN STRUCTURES AND INTEGRATED SYSTEMS, Vol. 56 (pp 534-544)
• Carniea G & Qin N (2008) Fluid-structure interaction of HALE wing configuration with an efficient moving grid method. 46th AIAA Aerospace Sciences Meeting and Exhibit(AIAA 2008-309). Reno, Nevada, 7 January 2008 - 10 January 2008.
• Elarbi E & Qin N (2008) Flapping dragonfly tandem wings and their practicalities to hovering micro aerial vehicles. The Aerodynamics of Novel configurations: capabilities and future requirements. Proceedings of the 2008 Royal Aeronautical Society Annual Applied Aerodynamics Research Conference. London, 27 October 2008 - 28 October 2008.
• Hamada K, Smith T, Durrani N, Qin N & Howell R (2008) . 46th AIAA Aerospace Sciences Meeting and Exhibit
• Edwards J, Durrani N, Howell R & Qin N (2008) Wind Tunnel and Numerical Study of a Small Vertical Axis Wind Turbine. 27th ASME Wind Energy Symposium(AIAA-2008-1316). Reno, Nevada, 7 January 2008 - 10 January 2008.
• Durrani N & Qin N (2008) Dynamic Mesh and Unsteady Flow for Flapping Airfoil with a Flexible Tail. 46th AIAA Aerospace Sciences Meeting and Exhibit(AIAA 2008-654). Reno, Nevada, 7 January 2008 - 10 January 2008.
• Hamada K, Smith T, Durrani N, Qin N & Howell R (2008) Unsteady flow simulation and dynamic stall around vertical axis wind turbine blades. 46th AIAA Aerospace Sciences Meeting and Exhibit
• Edwards J, Durrani N, Howell R & Qin N (2008) Wind tunnel and numerical study of a small vertical axis wind turbine. 46th AIAA Aerospace Sciences Meeting and Exhibit
• Durrani N & Qin N (2008) Numerical simulation of flexible flapping airfoil propulsion using dynamic mesh at low reynolds numbers. 46th AIAA Aerospace Sciences Meeting and Exhibit
• Xia H & Qin N (2008) DES applied to an isolated synthetic jet flow. ADVANCES IN HYBRID RANS-LES MODELLING (pp 252-260)
• Kuo CM, Boller C & Qin N (2007) Enhancing MAV Stability in Gusty Wind by Wing Flexibility: Analyses and Flight Tests. Unmanned Air Vehicle Systems. Bristol, UK, 16 April 2007 - 18 April 2007.
• Qin N, Wong WS & Le Moigne A (2007) Adjoint-based optimisation of a blended wing body aircraft with shock control bumps. Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting, Vol. 1(AIAA-2007-57) (pp 531-543). Reno, Nevada, 8 January 2007 - 11 January 2007.
• Xia H & Qin N (2006) Comparison of unsteady laminar and des solutions of synthetic jet flow. Collection of Technical Papers - AIAA Applied Aerodynamics Conference, Vol. 2(AIAA-2006-3161) (pp 878-888). San Francisco, California, 5 June 2006 - 8 June 2006.
• Le Moigne A & Qin N (2006) LES with numerical dissipation for aircraft wake vortices. Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting, Vol. 20(AIAA-2006-1258) (pp 15245-15257)
• Spence GT, Allerton DJ, Le Moigne A & Qin N (2005) Real-time model of wake vortices based on large eddy simulation datasets. Collection of Technical Papers - AIAA Modeling and Simulation Technologies Conference 2005, Vol. 1(AIAA-2005-6205) (pp 623-636). San Francisco, California,, 15 August 2005 - 18 August 2005.
• Wong WS, Qin N & Sellars ND (2005) A numerical study of transonic flow in a wind tunnel over 3D bumps. 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers(AIAA 2005-1057) (pp 161-169)
• Zhong B, Shaw ST & Qin N (2005) BILU implicit multiblock euler/navier-stokes simulation for helicopter rotor vortical flow. 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers(AIAA 2005-0465) (pp 2209-2222)
• Xia H & Qin N (2005) Dynamic grid and unsteady boundary conditions for synthetic jet flow. 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers(AIAA 2005-0106) (pp 4047-4055)
• Tadjouddine M, Forth S & Qin N (2005) Differentiating a Time-dependent CFD Solver. The ADCompEng Meeting. Shrivenham, UK, 23 June 2005 - 23 June 2005.
• Qin N, Wong WS, LeMoigne A & Sellars N (2005) Validation and optimisation od 3D bumps for transonic wing drag reduction. CEAS KATnet Conference on Key Aerodynamic Technologies. Bremen, Germany, 20 June 2005 - 22 June 2005.
• LeMoigne A & Qin N (2005) Large Eddy Simulation of Aircraft Wake Vortices on a Hybrid Grid. CEAS/KATnet Conference on Key Aerodynamic Technologies. Bremen, Germany, 20 June 2005 - 22 June 2005.
• Xia H & Qin N (2005) Detached-Eddy Simulation for Synthetic Jets in Cross-flows Using Dynamic Grid. CEAS/KATnet Conference on Key Aerodynamic Technologies. Bremen, Germany, 20 June 2005 - 22 June 2005.
• Xia H & Qin N (2005) Detached-eddy simulation for synthetic jets with moving boundaries,. 1st International Symposium on Physics of Fluids. Huangshan, China, 9 June 2005 - 12 June 2005.
• Qin N, Liu X & Xia H (2005) An efficient moving grid algorithm for large deformation. 1st International Symposium on Physics of Fluids. Huangshan, China, 9 June 2005 - 12 June 2005.
• Xia H & Qin N (2005) Dynamic grid solution of synthetic jets with oscillating membrane. RTO-MP-AVT-123 Flow-Induced Unsteady Loads and the Impact on Military Applications. Budapest, Hungery, 25 April 2005 - 28 April 2005.
• Shaw S, Hill J & Qin N (2005) . 43rd AIAA Aerospace Sciences Meeting and Exhibit
• Hill JL, Shaw ST & Qin N (2005) Development and application of engineering transition model for rotorcraft aerodynamics. 30th European Rotorcraft Forum, Vol. 2005 (pp 143-160)
• Hill J, Shaw ST & Qin N (2004) Investigation of transition modelling for aerofoil dynamic stall. ICAS 2004 CD-ROM PROCEEDINGS, 29 August 2004 - 3 September 2004.
• Le Moigne A & Qin N (2004) . 42nd AIAA Aerospace Sciences Meeting and Exhibit
• Qin N (2003) CFD for Better Understanding of Wind Tunnel Tests. First Symposium on Integrating CFD and Experiments in Aerodynamics. Glasgow, Scotland, UK, 8 September 2003 - 9 September 2003.
• Qin N, Vavalle A & Le Moigne A (2003) A study of spanwise lift distribution for blended wing body aircraft. CEAS Aerospace Aerodynamics Research Conference. Cambridge, UK, 3 June 2002 - 6 June 2002.
• Le Moigne A & Qin N (2003) A discrete adjoint method for aerodynamic sensitivities for Navier-Stokes flows. CEAS Aerodynamics Research Conference. Cambridge, UK
• Qin N, Vavalle A, LeMoigne A, Laban M, Hackett K & Weinerfelt P (2002) . AIAA Paper 2002-5448. Atlanta, Georgia, USA, 4 September 2002 - 6 September 2002.
• Qin N, Monet D & Shaw ST (2002) 3D bumps for transonic wing shock control and drag reduction. CD-ROM. London, 10 June 2002 - 13 June 2002.
• Birch TJ, Prince SA, Ludlow DK & Qin N (2001) The application of a parabolized navier-stokes solver to some hypersonic flow problems. 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference(AIAA 2001-1753)
• Perigo D & Qin N (2001) . 19th AIAA Applied Aerodynamics Conference(AIAA 2001-2417), 11 June 2001 - 14 June 2001.
• Qin N (2001) Experience with the Osher scheme for applied aerodynamics. GODUNOV METHODS: THEORY AND APPLICATIONS (pp 707-715)
• Qin N, Zhu Y, Ashill PR & Shaw ST (2000) . AIAA 18th Applied Aerodynamics Conference, Vol. Invited Paper on Active Flow Control(AIAA 2000-4329). Denver, USA, 14 August 2000 - 17 August 2000.
• Qin N & Lee S (2000) Viscous effects on transonic aeroelastic stability. Proceedings of the 4th Asian Computational Fluid Dynamics Conference, 18 September 2000 - 22 September 2000.
• Qin N & Chong Y (2000) Monotone integrated large eddy simulation for supersonic boundary layers. Proceedings of the 4th Asian Computational Fluid Dynamics Conference. Mianyang, China, 18 September 2000 - 22 September 2000.
• Zhong B & Qin N (2000) Non-inertial multiblock Navier-Stokes calculation for hovering rotor flowfields using high order approximate Riemann solver. Proceedings of the 4th Asian Computational Fluid Dynamics Conference. Mianyang, China, 18 September 2000 - 22 September 2000.
• Qin N, Ludlow DK & Shaw ST (2000) Matrix-free implicit methods for applied aerodynamics. Proceedings of the 4th Asian Computational Fluid Dynamics Conference(Invited paper). Mianyang, China, 18 September 2000 - 22 September 2000.
• Ludlow DK, Qin N & Birch TJ (2000) Towards a robust, efficient and accurate numerical solver for super/hypersonic flows over arbitrary geometries. ICAS 2000 CD-ROM PROCEEDINGS, 27 August 2000 - 1 September 2000.
• Prince S, Ludlow DK & Qin N (2000) Phantom vorticity in Euler solutions on highly stretched grids. ICAS 2000 CD-ROM PROCEEDINGS. Harrogate, UK, 27 August 2000 - 1 September 2000.
• Qin N, Zhu Y & Ashill P (2000) CFD study of shock control at Cranfield. ICAS 2000 CD-ROM PROCEEDINGS. Harrogate, UK, 27 August 2000 - 1 September 2000.
• Qin N & Perigo D (2000) A numerical investigation of the flows in and around annular plug nozzle configurations. ICAS 2000 CD-ROM PROCEEDINGS. Harrogate, UK, 27 August 2000 - 1 September 2000.
• Shaw ST & Qin N (2000) Direct calculation of compressible indicial response using CFD. Aerodynamics Conference 2000: RAeS Proceedings 399. London, 3 April 2000 - 3 April 2000.
• Qin N, Aurifeille EVJ & Shaw ST (2000) Vorticity curvature based algebraic turbulence model for unsteady synthetic jet flow around aerofoils. Aerodynamics Conference 2000: RAeS Proceedings 399. London
• Zhong B & Qin N (2000) Non-inertial multiblock Navier-Stokes calculation for hovering rotor flowfields using high order upwind scheme. Aerodynamics Conference 2000: RAeS Proceedings 399. London
• Shaw ST & Qin N (1999) A parametric study of the aerodynamics of inplane motion. Proceedings of the 25th European Rotorcraft Forum. Rome, 14 September 1999 - 16 September 1999.
• Prince SA, Qin N & Birch TJ (1999) Numerical investigation of the appearance of windward vortex shock about slender bodies. Proceedings of the 22nd International Symposium on Shock Waves. London, 18 July 1999 - 23 July 1999.
• Shaw ST & Qin N (1999) A numerical study of the relationship between steady and unsteady flow development for self-excited periodic flows. Proceedings of the 22nd International Symposium on Shock Waves. London, 18 July 1999 - 23 July 1999.
• Zhu Y & Qin N (1999) Inclined suction and blowing for shock control at transonic speeds. Proceedings of the 22nd International Symposium on Shock Waves. London, 18 July 1999 - 23 July 1999.
• Qin N & Ludlow DK (1999) Abnormalities of Osher and AUSM+ scheme for hypersonic flows around swept cylinders and a cure. Proceedings of the 22nd International Symposium on Shock Waves. London, 18 July 1999 - 23 July 1999.
• Kontis K, Qin N, Stollery JL & Edwards JA (1999) Lifting elliptic cones with and without strakes at hypersonic speeds. Proceedings of 10th Symposium on Shock Waves in JAPAN 1999, 19 March 1999 - 21 March 1999.
• Richardson G & Qin N (1999) . 37th Aerospace Sciences Meeting and Exhibit
• Qin N, Ludlow D, Zhong B & Shaw S (1999) . 37th Aerospace Sciences Meeting and Exhibit
• Qin N, Ludlow DK, Zhong B, Shaw ST & Birch TJ (1999) Multigrid acceleration of a preconditioned GMRES implicit PNS solver. 37th Aerospace Sciences Meeting and Exhibit
• Qin N & Jayatunga C (1998) Algebraic turbulence modelling for vortical flows around slender bodies. Proceedings of the AGARD 82nd Fluid Dynamics Panel Symposium on Missile Aerodynamics, Vol. AGARD CP-608(Paper 20). Sorrento
• Shaw S & Qin N (1998) . 36th AIAA Aerospace Sciences Meeting and Exhibit
• Ludlow D & Qin N (1998) . 36th AIAA Aerospace Sciences Meeting and Exhibit
• Qin N & Zhu Y (1998) . 36th AIAA Aerospace Sciences Meeting and Exhibit
• Richardson G & Qin N (1998) . 36th AIAA Aerospace Sciences Meeting and Exhibit
• Shaw S & Qin N (1998) A matrix-free preconditioned Krylov-subspace method for the PNS equations. 36th AIAA Aerospace Sciences Meeting and Exhibit
• (1998) Linear and non-linear turbulence models for shock-wave/ turbulent boundary-layer interaction using a strongly coupled approach. 36th AIAA Aerospace Sciences Meeting and Exhibit
• Qin N & Perigo D (1997) Numerical simulation of flows in and around clustered module plug nozzles. European Space Agency Advanced Nozzles Workshop. Rome, Italy, 13 October 1997 - 13 October 1997.
• Shaw ST & Qin N (1997) Numerical prediction of the aerodynamic response of aerofoils subject to step increases in Mach number. Proceedings of the 23nd European Rotorcraft Forum, Vol. 1 (pp 31.1-31.9)
• Qin N & Zhu Y (1997) Control of shock induced separation by surface suction. Proceedings of the 3rd Pacific International Conference on Aerospace Science and Technology (pp 204-210)
• Qin N, Stollery J, Kontis K, Qin N, Stollery J & Kontis K (1997) . 15th Applied Aerodynamics Conference
• Qin N, Zhu Y & Richardson G (1997) Structured grid adaptation and turbulence modelling for shock/boundary layer interactions. Proceedings of the 7th International Symposium on Computational Fluid Dynamics (pp 464-473)
• Richardson G & Qin N (1997) Solution of Delery’s transonic channel flow using the SST model. ECCOFTAC Workshop on Turbulence Models for Shock/Boundary Layer Interactions, 3 March 1997 - 3 March 1997.
• Qin N, Ludlow D, Shaw S, Edwards J, Dupuis A, Qin N, Ludlow D, Shaw S, Edwards J & Dupuis A (1997) . 35th Aerospace Sciences Meeting and Exhibit
• Richardson G, Qin N, Ludlow DK & Shaw ST (1997) Two equation turbulence modelling using a strongly coupled high resolution approach. RAeS 1997 Aerodynamics Research Forum. London, 6 January 1997 - 6 January 1997.
• Qin N, Ludlow OK, Shaw ST, Edwards JA & Dupuis A (1997) Calculation of pitch damping coefficients for projectiles. 35th Aerospace Sciences Meeting and Exhibit
• Qin N, Ludlow DK, Shaw ST & Richardson G (1997) A unified high resolution approach for two equation turbulence modelling. Proceedings of the 3rd Pacific International Conference on Aerospace Science and Technology (pp 219-225)
• Qin N & Redlich A (1996) . Fluid Dynamics Conference
• Shaw ST & Qin N (1996) Solution of the Navier-Stokes equations for the flow around an aerofoil in oscillating free stream. Proceeding of the 20th Congress of the International Council of the Aeronautical Sciences, Vol. 1 (pp 19-29)
• Qin N & Shaw ST (1996) Solution of Navier-Stokes equations for aerofoils undergoing combined translation-pitch oscillations. Proceedings of the 22nd European Rotorcraft Forum, Vol. 1 (pp 55.1-55.14)
• Qin N, Ludlow DK & Shaw ST (1996) A matrix-free Newton-GMRES method for steady and unsteady Navier-Stokes solutions. Proceedings of the 3rd ECCOMAS Computational Fluid Dynamics Conference (pp 784-790)
• Qin N & Foster G (1995) . Fluid Dynamics Conference
• Qin N & Foster GW (1994) CFD modelling of a transverse control jet. TTCP WTP-2 Conference(Paper 23.2)
• Birch TJ, Qin N & Jin X (1994) Computation of supersonic viscous flows around a slender body at incidence. AIAA 12th Applied Aerodynamic Conferenc(AIAA paper 94-1938)
• Qin N (1993) High resolution numerical simulation of transonic turbulent flow around RAE2822 airfoil. 9th International Conference on System Engineering. Las Vegas, USA
• XU X, QIN N & RICHARDS BE (1993) PARALLELIZING EXPLICIT AND FULLY IMPLICIT NAVIER-STOKES SOLUTIONS FOR COMPRESSIBLE FLOWS. PARALLEL COMPUTATIONAL FLUID DYNAMICS 92 (pp 407-418)
• QIN N, XU X & RICHARDS BE (1993) SFDN ALPHA-GMRES AND SQN ALPHA-GMRES METHODS FOR FAST HIGH-RESOLUTION N-S SIMULATIONS. NUMERICAL METHODS FOR FLUID DYNAMICS 4 (pp 583-592)
• Richards BE, Qin N, Xu X, Anderson JM & Bowman IMR (1992) Fast, accurate, robust Navier-Stokes solvers for hypersonic flows over configurations. The 1st Hypersonic Aerodynamic Advisory Group(HAAG) Meeting. London
• Xu X, Qin N & Richards BE (1992) Parallel alpha-GMRES solver and its application for Navier-Stokes equations. Proceedings of the Second Workshop on Parallel Numerical Analysis(EPCC-TR92-22). Edinburgh, UK
• Qin N, Anderson JM, Xu X & Richards BE (1992) Numerical modelling of the aerothermochemistry of spacecraft re-entry. Aerothermochemistry of spacecraft and associated hypersonic flows : proceedings of the IUTAM symposium (pp 228-235). Marseille, France, 1 September 1992 - 4 September 1992.
• Qin N, Xu X & Richards BE (1992) Newton-like methods for Navier-Stokes solution
• Qin N & Richards BE (1991) A study of hypersonic laminar/turbulent flow over a slender cone by the LCNS code. Workshop on Hypersonic Flows for Re-entry Problems, Vol. Part II, Vol 2 (pp 1-13)
• Qin N & Richards BE (1991) (pp 947-959)
• Chaudhry SR, Qin N & Richards BE (1990) Hypersonic viscous flows around waverider configurations. Proceedings of the 1st International Hypersonic Waverider Symposium. College Park, Maryland, U.S.A., 17 October 1990 - 19 October 1990.
• Qin N, Wang ZJ & Richards BE (1990) Numerical experiments using Navier-Stokes codes for generalised hypersonic shapes. Proceedings of the 17th Congress of the International Council of the Aeronautical Sciences, (pp 1927-1937)
• Qin N, Scriba KW & Richards BE (1989) Shock-shock, shock-vortex interaction and aerodynamic heating in hypersonic corner flow. Proceedings of the International Conference on Hypersonic Aerodynamics (pp 26.1-26.15). Manchester, UK
• Qin N & Richards BE (1989) A parallelised Navier-Stokes code combining high resolution with fast convergence. Validation of Methods for Computational Fluid Mechanics and Progress in Methods for Navier-Stokes an. Surrey, UK
• Qin N & Richards BE (1987) Prediction of the hypersonic flow on the leeside of a cone-delta-wing combination. Euromech 225: the Aerodynamics of Spacecraft. Cranfield, UK
• Qin N & Richards BE (1987) Numerical experiments with hypersonic flow beneath a cone-delta-wing combination. Proceedings of AGARD Conference on Aerodynamics of Hypersonic Lifting Vehicles, Vol. AGARD-CP-428 (pp 20.1-20.14)
• Qin N & Cao CP (1985) Semi-inverse iterative solution for the supersonic separated flows over a compression corner. Proceedings of the Third National Conference on Computational Fluid Dynamics
• Qin N & Cao CP (1985) A new numerical method for solving supersonic separated flows over a compression corner by introducing an interactive boundary condition. Proceedings of the Third National Conference on Computational Fluid Dynamics
• Bidar O, He P, Anderson S & Qin N () Turbulent Mean Flow Reconstruction Based on Sparse Multi-sensor Data and Adjoint-based Field Inversion. AIAA AVIATION 2022 Forum
• Bidar O, He P, Anderson S & Qin N () An open-source adjoint-based field inversion tool for data-driven RANS modelling. AIAA AVIATION 2022 Forum
• Qin N & Coppin J () Adjoint Based Aerodynamic Optimisation of a UCAV. AIAA Paper 2013-0146. Grapevine, Taxas, USA, 7 January 2013 - 13 January 2013.
• Qin N () Home Page

Patents

• Qin N, Shagpar S, Carnie GREG & Wang Y (2011) A Turbomachine Comprising an Annular Casing and a Bladed Rotor. GB Patent number 1101811.6 Appl. 01 May 2011.
• Shahpar S, Qin N, Wang Y & Carnie G (2011) A Method of Connecting Meshes. GB Patent number 1101810.8 Appl. 01 May 2011.
• Qin N (2010) Shock Control Vortex Generating Bumps. International Patent No WO 2011/098807 A1 Appl. 09 Feb 2010.
• Qin N (2010) Shock Control Vortex Generating Bumps. GB Patent No. GB1002281.2 Appl. 09 Feb 2010.
• Qin N, Alistair J & Shahpar S () nacelle intake. US20200102067A1 Appl. 01 Jan 1970.

Theses / Dissertations

• Qin N (1987) Towards numerical simulation of hypersonic flow around space-plane shapes. University of Glasgow.
• Bidar O Towards statistical inference to improve turbulence RANS closures for multi-element aerofoils.

Datasets

• Apetrei R, Ciobaca V, Sosa JC & Qin N .