Design methodology of an osculating cone waverider with adjustable sweep and dihedral angles
Author:
Funder
National Natural Science Foundation of China
the Natural Science Foundation of Hunan Province, China
Publisher
Zhejiang University Press
Subject
General Engineering
Link
https://link.springer.com/content/pdf/10.1631/jzus.A2000020.pdf
Reference41 articles.
1. Adamczak DW, Bolender MA, 2015. The flight dynamics of the HIFiRE Flight 6 research vehicle. Proceedings of AIAA Atmospheric Flight Mechanics Conference. https://doi.org/10.2514/6.2015-0528
2. Ding F, Shen CB, Liu J, et al., 2015a. 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
3. Ding F, Liu J, Shen CB, et al., 2015b. Novel approach for design of a waverider vehicle generated from axisymmetric supersonic flows past a pointed von Karman ogive. Aerospace Science and Technology, 42:297–308. https://doi.org/10.1016/j.ast.2015.01.025
4. Ding F, Liu J, Shen CB, et al., 2015c. Novel inlet-airframe integration methodology for hypersonic waverider vehicles. Acta Astronautica, 111:178–197. https://doi.org/10.1016/j.actaastro.2015.02.016
5. Ding F, Liu J, Shen CB, et al., 2015d. Simplified osculating cone method for design of a waverider. Proceedings of ASME Turbo Expo 2015: Turbine Technical Conference and Exposition.
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