Parameterization and optimization design of a hypersonic inward turning inlet
Author:
Funder
National Natural Science Foundation of China
CSC
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference24 articles.
1. Hypersonic Vehicle Design Using Inward Turing Flow Fields;Kothari,1996
2. An Overview of the Advantages and Concerns of Hypersonic Inward Turning Inlets;You,2011
3. Design of three-dimensional hypersonic inlets with rectangular-to-elliptical shape transition;Smart;J. Propuls. Power,1999
4. Design and experimental study of a practical osculating inward cone waverider inlet;He;Chin. J. Aeronaut.,2016
5. Novel approach for designing a hypersonic gliding-cruising dual waverider vehicle;Liu;Acta Astronaut.,2014
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