Research on Drag Reduction and Heat Prevention of Supersonic Vehicle with the Composite Configuration of Spike and Lateral Jet-Reference-Cited by-同舟云学术

Research on Drag Reduction and Heat Prevention of Supersonic Vehicle with the Composite Configuration of Spike and Lateral Jet

Published:2022-06-24 Issue: Volume: Page:
ISSN:
Container-title:2022 the 14th International Conference on Computer Modeling and Simulation
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Author:

Wang Ziyu¹,Fang Shuzhou¹,Xu Yang¹

Affiliation:

1. School of Aerospace Engineering, Beijing Institute of Technology, China

Publisher

ACM

Link

https://dl.acm.org/doi/pdf/10.1145/3547578.3547597

Reference13 articles.

1. Yang Y Z Y J L , Fang D N . Research progress on thermal protection materials and structures of hypersonic vehicles[J]. Applied Mathematics and mechanics (English version) , 2008 , 29(1): 51-60. Yang Y Z Y J L, Fang D N. Research progress on thermal protection materials and structures of hypersonic vehicles[J]. Applied Mathematics and mechanics (English version), 2008, 29(1): 51-60.

2. Schmisseur J D . Hypersonics into the 21st century: A perspective on AFOSR-sponsored research in aerothermodynamics[J]. Progress in aerospace sciences , 2015 , 72(Jan.): 3-16. Schmisseur J D. Hypersonics into the 21st century: A perspective on AFOSR-sponsored research in aerothermodynamics[J]. Progress in aerospace sciences, 2015, 72(Jan.): 3-16.

3. Shock Wave Drag Reduction

4. Experimental investigation on aerothermal effects of forward-facing cylindrical and parabolic cavity in hypersonic flow

5. Drag and heat flux reduction mechanism induced by the combinational forward-facing cavity and pulsed counterflowing jet configuration in supersonic flows

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