Three-dimensional numerical study on reducing hypersonic blunt body drag and aeroheating with spike-aerodisk-bleed air channel-Reference-Cited by-同舟云学术

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Three-dimensional numerical study on reducing hypersonic blunt body drag and aeroheating with spike-aerodisk-bleed air channel

Published:2024-02 Issue: Volume:215 Page:674-688
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Ni Zijian,Fang Shuzhou^ORCID,Guo Jian,Wang Ziyu,xu Yang

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference51 articles.

1. Aerothermodynamics of blunt body entry vehicles;Hollis;Prog.Aerosp. Sci.,2012

2. A review of design issues specific to hypersonic flight vehicles;Sziroczak;Prog. Aero. Sci.,2016

3. Shock wave drag reduction;Bushnell;Annu. Rev. Fluid Mech.,2004

4. Drag and heat reduction mechanism in the combinational opposing jet and acoustic cavity concept for hypersonic vehicles;Huang;Aero. Sci. Technol.,2015

5. Experimental and numerical study on the aero-heating characteristics of blunted waverider;Liu;Appl. Therm. Eng.,2013

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1. Numerical investigation of blunt body's resistance and heat reduction with combination of airway spike and root jet;International Journal of Thermal Sciences;2024-09

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