- Moss, J.N., Glass,C.E., and Greenez, F.A. “DSMC Simulations of Apollo Capsule Aerodynamics for Hypersonic Rarefied Conditions”, The 9th AIAA Joint Thermophysics and Heat Transfer Conf., San Francisco, California, 2006.
- Ivanov, M.S., Vashchenkov, P., and Kashkovsky, A. “Numerical Investigation of the EXPERT Reentry Vehicle Aerothermodynamics along the Descent Trajectory”, The 39th AIAA Thermophysics Conf., 2007.
- Zuppardi, G., Morsa, L., Schettino, A., Votta, R., Levin, D.A., Wysong, I.J., & Garcia,A.L. “Analysis of Aero-Thermodynamic Behavior of Expert Capsule in Transitional Regime”, In AIP Conf., American Institute of Physics, Vol. 1333, No. 1, p. 1349, 2011.
- Liu, J., Ding, F., Huang, W., and Jin, L. “Novel Approach for Designing a Hypersonic Gliding–Cruising Dual Waverider Vehicle”, Acta Astronautica, Vol. 102, pp. 81-88, 2014.
- Nonweiler, T.R.F. “Delta Wings of Shapes Amenable to Exact Shock-Wave Theory”, J. Royal Aeronautical Society, Vol. 67, pp. 39-40, 1963.
- Jones, M.J., Moore, M. K., Pike, M.J., and Roe, M.P. “A Method for Designing Lifting Configurations for High Supersonic Speeds, Using Axisymmetric Flow Fields”, Ingenieur-Archiv, Vol. 37, pp. 56-72, 1968.
- Rasmussen, M.P.F. ”Waverider Configurations Derived from Inclined Circular and Elliptic Cones”, J. Spacecraft and Rockets, Vol. 17, pp. 537-545, 1980.
- Corda, S. and Anderson, J. “Viscous Optimized Hypersonic Waveriders Designed from Axisymmetric Flow Fields”, The 26th AIAA Aerospace Sciences Meeting, Reno, NV, 1988.
- Xuzhao, H. and Le Jialing, W.Y. “Design of a Curved Cone Derived Waverider Forebody”, The 16th AIAA/DLR/DGLR Int. Space Planes and Hypersonic Systems and Technologies, 2009.
- Goonko, Y.P., Mazhul, I.I., and Markelov, G.N. “Convergent-Flow- Derived Waveriders”, J. Aircraft, Vol. 37, pp. 647-654, 2000.
- Mazhul, I.I. “Off-design Regimes of Flow Past Wave Riders, Based on Isentropic Compression Flows”, Fluid Dynamics, Vol. 45, pp. 271-280, 2010.
- Takashima, N. and Lewis, M.J. “Waverider Configurations, Based on Non-Axisymmetric Flow Fields for Engine-Airframe Integration”, The 32nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 1994.
- Bird, G.A. “Molecular Gas Dynamics and Direct Simulation of Gas Flows”, Oxford University Press, Oxford, 1994.
- Bird, G.A. “The DSMC method”, Create Space Independent Platform, Portsmouth, NH, USA, 2013.
- Bird, G.A. “The DS2V Program User’s Guide Ver. 3.2.”, GAB Consulting Pty Ltd., Sydney, Australia, 2005.
- Bird, G.A. “Visual DSMC Program for Three-dimensional Flows: The DS3V Program User’s Guide”, 2006.
- Anderson, J.D. “Hypersonic and High Temperature Gas Dynamics”, NY: McGraw-Hill, 1989.
- Eggers, A.J. and Syvertson, C.A. “Aircraft Configurations Developing High Lift-Drag Ratios at High Supersonic Speeds”, NACA RM-A55L05, 1956.
- Qu, Z.H. “Hypersonic Aerodynamics”, National University of Defense Technology Press, Changsha, 2000.
- Lin, T.C., Grabowsky, W.R., and Yelmgren, K.E. “The Search For Optimum Configurations for Re-Entry Vehicles”, J. Spacecraft and Rockets, Vol 21, No. 2, pp. 142-149, 1984.
- Stetson, K.F. and Lewis, A.B. “Aerodynamic Comparison of a Conical and Biconic Reentry Vehicle”, AIAA Preprint, pp. 77-1161, 1977.
- Roohi. E. and Stefanov. S. "Collision Partner Selection Schemes in DSMC: From Micro/Nano Flows to Hypersonic Flows." Physics Reports, pp. 1-38, 2016.
- Le, Nam TP. and Ngoc Anh Vu. "Effect of the Sliding Friction On Heat Transfer In High-Speed Rarefied Gas Flow Simulations in CFD." Int. J. Thermal Sciences, pp. 334-341, 2016.
- Knight, D. “RTO WG 10: Test Cases for CFD Validation of Hypersonic Flight”, AIAA 2002-0433, American Institute of Aeronautics and Astronautics, Reston, VA, 2003.
- Holden, M.S., Wadhams, T.P., Candler, G.V., Harvey, J.K., “Measurements of Regions of Low Density Laminar Shock Wave/Boundary Layer Interactions in Hypersonic Flows and Comparison with Navier-Stokes Predictions”, AIAA, 2003.
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