[1] DIETRICH K. The aerodynamic design of aircraft:AIAA-2012-0448[R]. Reston, VA:AIAA, 2012. [2] NONWEILER T R F. Aerodynamic problems of manned space vehicles[J]. Aeronautical Journal, 1959, 63(585):521-528. [3] JONES J G, MOORE K C, PIKE J, et al. A method fo designing lifting configurations for high supersonic speeds using axisymmetric flow field[J]. Archive of Applied Mechanics, 1968, 37(1):56-72. [4] RASMUSSEN M L. Waverider configurations derived from inclined circular and elliptic cones[J]. Journal of Spacecraft and Rockets, 1980, 17(6):537-545. [5] LOBBIA M A, SUZZKI K. Experimental investiga-tion of a Mach 3.5 waverider designed using computa-tional fluid dynamics[J]. AIAA Journal, 2015, 53(6):1590-1601. [6] SOBIECZKY H, DOUGHERTY F C, JONES K. Hyper-sonic waverider design from given shock waves[C]//In-ternational Hypersonic Waverider Symposium, 1990. [7] MILLER D S, WOOD R M. Lee-side flow over delta wings at supersonic speed:NASA TP-2430[R]. Washington, D.C.:NASA, 1985. [8] STARKEY R, LEWIS M. A simple analytical model for parametric studies of hypersonic waveriders:AIAA-1998-1616[R]. Reston, VA:AIAA, 1998. [9] RODI E P. The osculating flowfield method of waverider geometry generation:AIAA-2005-0511[R]. Reston, VA:AIAA, 2005. [10] RODI E P. Geometrical relationships for osculating cones and osculating flowfield waveriders:AIAA-2011-1188[R]. Reston, VA:AIAA, 2011. [11] MOELDER S. Internal, axisymmetric, conical flow[J]. AIAA Journal, 1967, 5(7):1252-1255. [12] 刘传振, 白鹏, 陈冰雁. 双后掠乘波体设计及性能优势分析[J]. 航空学报, 2017, 38(6):120808. LIU C Z, BAI P, CHEN B Y. Design and property advantages analysis of double swept waverider[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(6):120808(in Chinese). [13] HUANG X Z, MEBARKI Y, BENMEDDOUR A, et al. Experimental and numerical studies of geometry effects on UCAV's aerodynamics:AIAA-2004-0403[R]. Reston, VA:AIAA, 2004. [14] ROE P L. Approximate Riemann solvers, parameter vectors, and difference schemes[J]. Journal of Computational Physics, 1981, 43:357-372. [15] VENKATA KRISHNAN V. On the accuracy of limiters and convergence to steady state solutions:AIAA-1993-0880[R]. Reston, VA:AIAA, 1993. [16] KERMANI M J, PLETT E G. Modified entropy correction formula for the Roe scheme:AIAA-2001-0083[R]. Reston, VA:AIAA, 2001. [17] MENTER F R. Two-equation eddy-viscosity turbulence models for engineering applications[J]. AIAA Journal, 1994, 32(8):1598-1605. [18] WANG Z J, CHEN R F. Fast, block lower-upper Symmet-ric Gauss-Seidel scheme for arbitrary grids[J]. AIAA Journal, 2000, 38(12):2238-2245. [19] BOWCUTT K G. Optimization of hypersonic waveriders derived from cone flows-Including viscous effects[D]. Maryland:University of Maryland, 1986. [20] PATRICK E R. Vortex lift waverider configurations:AIAA-2012-1238[R]. Reston, VA:AIAA, 2012. |