Conversion of hydrocarbon fuel in a thermal protection reactors of hypersonic aircraft
A.L. Kuranov, A.V. Korabelnikov and A.M. Mikhailov
Plasma control of sock wave configuration in M=2 inlet at off-design mode
S. Leonov, F. Falempin, M.A. Goldfeld and A. Firsov
Research on Hypersonic Inlet Leading Edge Radius Effect on Wall Static Pressure and Heat Flux
Z. Wang, H. Bai and K. Zhang
Numerical Prediction and Experimental Verification of Shock Oscillation for a Hypersonic Inlet at Low Supersonic Mach Numbers
A.Y. Yu, D.W. Yang, J. Wu, H.L. Ni and J.L. Le
The Design and Study of Osculating Curved Cone Waverider-based Airbreathing Integrated Hypersonic Vehicle
H.E. Yuanyuan, W.U. Yingchuan, Y.U. Anyuan, H. Wei and L. Jialing
Numerical Investigation on the Start/Unstart Performance of a Supersonic Inlet
S.B. Li, S.B. Luo, W. Huang, Z. G. Wang and L. Yan
A Numerical Investigation of Air Intakes for the 14-X Hypersonic Vehicle Scramjet Engine
A. F. Moura and M. A. Rosa
Air Intake Design for the Acceleration Propulsion Unit of the LAPCAT MR2 Hypersonic Aircraft (*)
C. Meerts and J. Steelant
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