1.O’Neill, M.K. Optimized scramjet engine integration on a waverider airframe, Ph.D., University of Maryland College Park, College Park, MD, 1992.
2.O’Neill, M.K. and Lewis, M.J. Optimized scramjet integration on a waverider, J Aircraft 1992, 29, (6), pp 1114–1121.
3.You, Y.C., Liang, D.W., Guo, R.W. and Huang, G.P. Overview of the integration of three-dimensional inward-turning hypersonic inlet and waverider forebody, Adv Mech, 2009, 39, (5), pp 513–525 (in Chinese).
4.Ding, F., Liu, J., Shen, C.-B. and Huang, W. Novel inlet-airframe integration methodology for hypersonic waverider vehicles, Acta Astronaut, 2015, 111, pp 178–197.
5.Heiser, W.H. and Pratt, D.T. Hypersonic airbreathing propulsion, AIAA Inc., USA, 1994, pp 24–26.
6.Haney, J.W. and Beaulieu, W.D. Waverider inlet integration issues, AIAA Paper 94–0383, 1994.
7.Nonweiler, T.R.F. Aerodynamic problems of manned space vehicles, J Royal Aeronaut Soc, 1959, 63, pp 521–528.
8.Liu, J., Ding, F., Huang, W. and Jin, L. Novel approach for designing a hypersonic gliding-cruising dual waverider vehicle, Acta Astronaut, 2014, 102, pp 81–88.
9.Ding, F., Shen, C.-B., Liu, J. and Huang, W. Influence of surface pressure distribution of basic flow field on shape and performance of waverider, Acta Astronaut, 2015, 108, pp 62–78.
10.Ding, F., Liu, J., Shen, C.-B. and Huang, W. Novel approach for design of a waverider vehicle generated from axisymmetric supersonic flows past a pointed von Karman ogive, Aerosp Sci Technol, 2015, 42, pp 297–308.
11.Ding, F., Shen, C.-B., Liu, J. and Huang, W. Comparison between novel waverider generated from flow past a pointed von Karman ogive and conventional cone-derived waverider, Proc IMechE Part G: J Aerosp Eng, 2015, 229, (14), pp 2620–2633.
12.Lobbia, M.A. and Suzuki, K. Experimental investigation of a Mach 3.5 waverider designed using computaional fluid dynamics, AIAA J, 2015, 53, (6), pp 1590–1601.
13.Cui, K., Li, G.-L., Xiao, Y. and Xu, Y.-Z. High-pressure capturing wing configurations, AIAA J, 2017, 55, (6), pp 1909–1919.
14.Ding, F., Liu, J., Shen, C.-B., Liu, Z., Chen, S.-B. and Fu, X. An overview of research on waverider design methodology, Acta Astronaut, 2017, 140, pp 190–205.
15.Lewis, M.J. Application of waverider-based configurations to hypersonic vehicle design, AIAA Paper 91–3304, 1991.
16.Stevens, D.R. Practical considerations in waverider applications, AIAA Paper 92–4247, 1992.
17.Ding, F., Liu, J., Shen, C.-B., Huang, W., Liu, Z. and Chen, S.-H. An overview of waverider design concept in airframe/inlet integration methodology for air-breathing hypersonic vehicles, Acta Astronaut, 2018, 152, pp 639–656.
18.Starkey, R.P. and Lewis, M.J. Critical design issues for airbreathing hypersonic waverider missiles, J Spacecraft and Rockets, 2001, 38, (4), pp 510–519.
19.Starkey, R.P. and Lewis, M.J. Aerodynamics of a box constrained waverider missile using multiple scramjets, AIAA Paper 99–2378, 1999.
20.Starkey, R.P., Rankins, F. and Pines, D. Coupled waverider/trajectory optimization for hypersonic cruise, AIAA Paper 2005–530, 2005.
21.Li, Y.Q., Han, W.Q. and You, Y.C. Integration waverider design of hypersonic inlet and forebody with preassigned pressure distirbution, Acta Aeronaut Astronaut Sin, 2016, 37, (9), pp 2711–2720 (in Chinese).
22.Javaid, K.H. and Serghides, V.C. Airframe-propulsion integration methodology for waverider-derived hypersonic cruise aircraft design concepts, J Spacecr Rocket, 2005, 42, (4), pp 663–671.
23.Javaid, K.H. and Serghides, V.C. Thrust-matching requirements for the conceptual design of hypersonic waverider vehicles, J Aircraft, 2005, 42, (4), pp 1055–1064.
24.Lobbia, M. and Suzuki, K. Numerical investigation of waverider-derived hypersonic transport configurations, AIAA Paper 2003–3804, 2003.
25.Takashima, N. and Lewis, M.J. Engine-airframe integration on osculating cone waverider-based vehicle designs. AIAA Paper 96–2551, 1996.
26.O’Brien, T.F. RBCC engine-airframe integration on an osculating cone waverider vehicle, Ph.D., University of Maryland College Park, College Park, MD, 2001.
27.O’Brien, T.F. and Lewis, M.J. RBCC engine-airframe integration on an osculating cone waverider vehicle, AIAA Paper 2000–3823, 2000.
28.O’Brien, T.F. and Lewis, M.J. Rocket-based combined-cycle engine integration on an osculating cone waverider vehicle, J Aircraft, 2001, 38, (6), pp 1117–1123.
29.Lyu, Z.J. and Wang, J.F. Design and comparative analysis of multistage compression cone-derived waverider and osculating cone waverider, J Beijing Univ Aeronaut Astronaut, 2015, 41, (11), pp 2103–2109 (in Chinese).
30.Wang, X.D., Wang, J.F. and Lyu, Z.J. A new integration method based on the coupling of mutistage osculating cones waverider and Busemann inlet for hypersonic airbreathing vehicles, Acta Astronaut, 2016, 126, pp 424–438.
31.He, X.Z., Le, J.L. and Wu, Y.C. Design of a curved cone derived waverider forebody, AIAA Paper 2009–7423, 2009.
32.He, X.Z., Le, J.L., Zhou, Z., Mao, P.F. and Wu, Y.C. Osculating inward turning cone waverider/inlet (OICWI) design methods and experimental study, AIAA Paper 2012–5810, 2012.
33.He, X.Z., Le, J.L., Zhou, Z. and Wei, F. Progress in waverider inlet integration study, AIAA Paper 2015–3685, 2015.
34.He, X.Z., Zhou, Z., Qin, S., Wei, F. and Le, J.L. Design and experimental study of a practical osculating inward cone waverider inlet, Chinese J Aeronaut, 2016, 29, (6), pp 1582–1590.
35.Rodi, P.E. Engineering-based performance comparisons between osculating cone and osculating flowfield waveriders, AIAA Paper 2007–4344, 2007.
36.Rodi, P.E. Preliminary ramjet/scramjet integration with vehicles using osculating flowfields waverider forebodies, AIAA Paper 2012–3223, 2012.
37.You, Y.C., Zhu, C.X. and Guo, J.L. Dual waverider concept for the integration of hypersonic inward-turning inlet and airframe forebody, AIAA Paper 2009–7421, 2009.
38.Li, Y.Q., An, P., Pan, C.J., Chen, R.Q. and You, Y.C. Integration methodology for waverider-derived hypersonic inlet and vehicle forebody, AIAA Paper 2014–3229, 2014.
39.Cui, K., Hu, S.C., Li, G.L., Qu, Z.P. and Situ, M. Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets. Sci China Technol Sci, 2013, 56, (8), pp 1980–1988.
40.Atamanchuk, T., Sislian, J. and Dudebout, R. An aerospace plane as a detonation wave ramjet/airframe integrated waverider, AIAA Paper 92–5022, 1992.
41.Tarpley, C., and Lewis, M.J. Optimization of an engine-integrated waverider with steady state flight constraints. AIAA Paper 95–0848, 1995.
42.Tarpley, C. The optimization of engine-integrated hypersonic waveriders with steady state flight and static margin constraints, Ph.D., University of Maryland College Park, College Park, MD, 1995.
43.Newberry, C.F. The conceptual design of deck-launched waverider configured aircraft, AIAA Paper 95–6155, 1995.
44.Takashima, N. and Lewis, M.J. Optimization of waverider-based hypersonic cruise vehicles with off-design considerations, J Aircraft, 1999, 36, (1), pp 235–245.
45.Takashima, N. Optimization of waverider-based hypersonic vehicle designs, Ph.D., University of Maryland, College Park, 1997.
46.Zucrow, M.J. and Hoffman, J.D. Gas Dynamics, Vol. 2: Multidimensional Flow, John Wiley and Sons, Inc., New York, 1977, pp 112–266.
47.Kothari, A.P., Tarpley, C., Mclaughlin, T.A., Babu, B.S. and Livingston, J.W. Hypersonic vehicle design using inward turning flow fields, AIAA Paper 96–2552, 1996.
48.Billig, F.S. and Kothari, A.P. Streamline tracing: technique for designing hypersonic vehicles, J Propuls Power, 2000, 16, (3), pp 465–471.
49.Fluent Inc., ANSYS FLUENT 13.0 Theory Guide, ANSYS, Inc., 2010.
50.Barth, T.J. and Jespersen, D. The design and application of upwind schemes on unstructured meshes, AIAA Paper 89–0366, 1989.
51.Huang, W., Wang, Z.G., Pourkashanian, M., Ma, L., Ingham, D.B., Luo, S.B., Lei, J. and Liu, J. Numerical investigation on the shock wave transition in a three-dimensional scramjet isolator, Acta Astronaut, 2011, 68, pp 1669–1675.
52.Huang, W. and Wang, Z.G. Numerical study of attack angle characteristics for integrated hypersonic vehicle, Appl Math Mech (Engl Ed), 2009, 30, (6), pp 779–786.
53.Huang, W., Liu, W.D., Li, S.B., Xia, Z.X., Liu, J. and Wang, Z.G., Influences of the turbulence model and the slot width on the transverse slot injection flow field in supersonic flows, Acta Astronaut, 2012, 73, pp 1–9.
54.Mansour, K. and Khorsandi, M. The drag reduction in spherical spiked blunt body, Acta Astronaut, 2014, 99, pp 92–98.
55.Chen, X.Q., Hou, Z.X., Liu, J.X. and Gao, X.Z. Bluntness impact on performance of waverider, Comput. Fluids, 2011, 48, pp 30–43.
56.Liu, J.X., Hou, Z.X., Chen, X.Q. and Zhang, J.T. Experimental and numerical study on the aero-heating characteristics of blunted waverider, Appl. Therm Eng, 2013, 51, pp 301–314.
57.Roy, C.J. and Blottner, F.G. Review and assessment of turbulence models for hypersonic flows, Prog. Aerosp. Sci, 2006, 42, pp 469–530.
58.Reinartz, B.U., Herrmann, C.D. and Ballmann, J. Aerodyanmic performance analysis of a hypersonic inlet isolator using computation and experiment, J. Propuls Power, 2003, 19, (5), pp 868–875.
59.Ding, F., Shen, C.-B., Huang, W. and Liu, J. Numerical validation and back-pressure effect on internal compression flows of typical supersonic inlet, Aeronaut J, 2015, 119, (1215), pp 631–645.
60.Schmitz, D.M. and Bissinger, N.C. Design and testing of 2-D fixed-geometry hypersonic intakes, AIAA Paper 98–1529, 1998.
61.Huang, P.G. and Coakley, T.J. Turbulence modeling for complex hypersonic flows, AIAA Paper 93–0200, 1993.
62.Li, S.X. The flow characteristics for the typical model in hypersonic flows, National Defence Industry Press, Beijing, 2007.