Design methodology of the hypersonic axisymmetric forebody
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference22 articles.
1. 3D inverse method of characteristics for hypersonic bump-inlet integration;Yu;Acta Astronaut.,2020
2. Numerical investigation on behaviors of shock train in a hypersonic inlet with translating cowl;Shi;Acta Astronaut.,2018
3. Design methodology of the waverider with a controllable planar shape;Wang;Acta Astronaut.,2018
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