Design and numerical simulation of a clamshell-shaped inlet cover for air-breathing hypersonic vehicles
Author:
Funder
National Natural Science Foundation of China
the Joint Funds of the National Natural Science Foundation of China
Publisher
Zhejiang University Press
Subject
General Engineering
Link
http://link.springer.com/content/pdf/10.1631/jzus.A1800620.pdf
Reference21 articles.
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2. Brauckmann GJ, Streett C, Kleb WL, et al., 2015. Computational and experimental unsteady pressures for alternate SLS booster nose shapes. Proceedings of the 53rd AIAA Aerospace Sciences Meeting. https://doi.org/10.2514/6.2015-0559
3. Colonno MR, Alonso JJ, 2008. The optimum launch vehicle fairing: an MDO approach. Proceedings of the 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. https://doi.org/10.2514A5.2008-5883
4. Ding F, Shen CB, Liu J, et al., 2015. Influence of surface pressure distribution of basic flow field on shape and performance of waverider. Acta Astronautica, 108:62–78. https://doi.org/10.1016/j.actaastro.2014.11.038
5. Groves CE, Ilie M, Schallhorn PA, 2014. Computational fluid dynamics uncertainty analysis for payload fairing spacecraft environmental control systems. Proceedings of the 52nd Aerospace Sciences Meeting. https://doi.org/10.2514/6.2014-0440
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