Design, Modeling and Analysis of a Sharp-edge Hypersonic Stealthy Re-entry Vehicle
Author:
Publisher
Elsevier BV
Subject
Applied Mathematics
Reference15 articles.
1. Böhrk H, Dittert C, Tiele T, et al. Thermal testing of the sharp leading edge of SHEFEX-II[C]. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. 2012.
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3. Barth T. Aerothermodynamic analysis to SHEFEX I[J]. Engineering Applications of Computational Fluid Mechanics. 2007, 1(1): 76-84.
4. Eggers T, Stamminger A, Hörschgen M, et al. The hypersonic experiment SHEFEX aerothermodynamic layout, vehicle development and first flight results[C]. Proceedings of 6th International Symposium on Launcher Technologies ‘Flight Environment Control for Future and Operational Launchers’.2005.
5. Dietlein I, Kopp A. System analysis for “sharp-edge” re-entry vehicles[C]. AIAA 2009-7427.
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