| Citation: | CHEN Xue-dong, WANG Fa-min. Aerodynamic characteristics of waverider and its integrated configuration with blunt leading edge[J]. Journal of Aerospace Power, 2013, 28(2): 379-384.
|
| [1] |
解发瑜,李刚,徐忠昌.高超声速飞行器概念及发展动态[J].飞航导弹,2004(5):27-31.
|
| [2] |
朱云骥,史忠科.高超声速飞行器飞行特性和控制的若干问题[J].飞行力学,2005,23(3):5-8. ZHU Yunji,SHI Zhongke.Several problems of flight characteristics and flight control for hypersonic vehicles[J].Flight Dynamics,2005,23(3):5-8.(in Chinese)
|
| [3] |
Engelund W C,Holland S C,Charles E C,Jr,et al.Propulsion system airframe integration issues and aerodynamic database development for the hyper-X flight research vehicle[R].Hampton,VA,US:NASA,XIV ISOABE 99-7215,1999.
|
| [4] |
唐硕,祝强军.吸气式高超声速飞行器动力学建模研究进展[J].力学进展,2011,41(2):187-200. TANG Shuo,ZHU Qiangjun.Research progresses on flight dynamics modeling of airbreathing hypersonic flight vehicles[J].Advances in Mechanics,2011,41(2):187-200.(in Chinese)
|
| [5] |
Nonweiler T R F.Delta wings of shape amenable to exact shock-wave theory[J].Journal of the Royal Aeronautical Society,1963,67:39-40.
|
| [6] |
Bowcutt K G,Anderson J D.Viscous optimized hypersonic waveriders[R].AIAA-87-0272,1987.
|
| [7] |
Corda S,Anderson J D.Viscous optimized hypersonic waveriders deigned from axisymmetric flow fields[R].AIAA-88-0369,1988.
|
| [8] |
O'Neill M K,Lewis M J.Optimized scramjet integration on waverider[R].AIAA-91-1693,1991.
|
| [9] |
Starkey R P,Lewis M J.Design of an engine-airframe integrated hypersonic missile within foxed box constraints[R].AIAA-99-0509,1999.
|
| [10] |
Starkey R P,Lewis M J.Performance of hypersonic waverider missiles using multiple scramjets[R].AIAA-99-4953,1999.
|
| [11] |
Starkey R P,Lewis M J.Critical design issues for airbreathing hypersonic waverider missiles[J].Journal of Spacecraft and Rockets,2001,38(4):510-519.
|
| [12] |
潘静.高超声速飞行器气动防热新概念研究[J].力学学报,2010,42(3):383-388. PAN Jing.New conception of aerothermal protection for hypersonic vehicles[J].Acta Mechanica Sinica,2010,42(3):383-388.(in Chinese)
|
| [13] |
Vinogradov V,Stepanov V,Goldfeld M.Experimental and uumerical investigation of two concepts of the hypersonic inlet[R].AIAA-95-2721,1995.
|
| [14] |
Auneau I,Garnero P,Doveau P.Design and optimization methods for scramjets inlets[R].AIAA-95-6017,1995.
|
| [15] |
韩兆林,王强.双模态冲压发动机进气道/隔离段流场的数值研究[J].航空动力学报,2006,21(1):31-35. HAN Zhaolin,WANG Qiang.Numerical investigation on inlet/isolator flow field of a dual-mode scramjet[J].Journal of Aerospace Power,2006,21(1):31-35.(in Chinese)
|
| [16] |
罗世彬,罗文彩,丁猛,等.超燃冲压发动机二维进气道多级多目标优化设计方法[J].国防科技大学学报,2004,26(3):1-6. LUO Shibin,LUO Wencai,DING Meng,et al.The multi-level and multiobjective optimization design method for two dimensional scramjet inlet[J].Journal of National University of Defense Technology,2004,26(3):1-6.
|
| [17] |
李淑艳.高超声速进气道设计及性能研究[R].西安:西北工业大学,2006.
|
DownLoad: