Active impact on the flow around hypersonic flying vehicles

Author:

Borisov Vitaly Evgenyevich1ORCID,Lutsky Alexander Evgenievich1,Severin Alexander Vladimirovich1,Khankhasaeva Yana Vladislavovna1

Affiliation:

1. Keldysh Institute of Applied Mathematics

Publisher

Keldysh Institute of Applied Mathematics

Subject

General Medicine

Reference22 articles.

1. E.G. Prisell, The Feasibility of the Scramjet; an Analysis Based on First Principles // 25th International Congress of the Aeronautical Sciences, ICAS 2006, pp. 1-14.

2. C.R. McClinton, High Speed/Hypersonic Aircraft Propulsion Technology Development. In Advances on Propulsion Technology for High-Speed Aircraft. Educational Notes RTO-EN-AVT-150, Paper 1. 2008. Neuilly-sur-Seine, France: RTO. pp 1-32.

3. D.E. Reubush, L.T. Nguyen, V.L. Rausch, Review of X-43A Return to Flight Activities and Current Status // AIAA 2003-7085. 2003. 12 p.

4. J.P. Drummound, M. Bouchez, C.R. McClinton, Overview of NATO Background on Scramjet Technology // NATO report. 2002.

5. L.D. Huebner, K.E. Rock, E.G. Ruf, D.W. Witte and E.H. Andrews, Hyper-X Flight Engine Ground Testing for Flight Risk Reduction // Journal of Spacecraft and Rockets, Vol. 38, No. 6 (2001), pp. 844-852. http://dx.doi.org/10.2514/2.3774

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