Heat flux in supersonic flow past ballistic model at various angles of attack and wall temperatures-Reference-Cited by-同舟云学术

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Heat flux in supersonic flow past ballistic model at various angles of attack and wall temperatures

Published:2021-06 Issue: Volume:183 Page:52-58
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Borisov V.E.^ORCID,Chetverushkin B.N.,Davydov A.A.,Khankhasaeva Ya.V.^ORCID,Lutskii A.E.^ORCID

Funder

Russian Science Foundation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference30 articles.

1. Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles;Hirschel,2009

2. Comparative Force/Heat Flux Measurements between JAXA Hypersonic Test Facilities Using Standard Model HB-2;Kuchi-Ishi,2005

3. Summary Report on Aerodynamic Characteristics of Standard Models HB-1 and HB-2;Gray,1964

4. Short duration force measurements in impulse facilities;Robinson,2006

5. Pressure Tests on the Standard Hypervelocity Ballistic Model HB-2 at Mach 1.5 to 5;Jones,1964

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1. Formation of Shock-Wave Flow during Nanosecond Discharge Localization in Unsteady Flow in a Channel with Obstacles;Fluid Dynamics;2023-02

2. Formation of Shock-Wave Flow during Nanosecond Discharge Localization in Unsteady Flow in a Channel with Obstacles;Известия Российской академии наук. Механика жидкости и газа;2023-01-01

3. Some Features of DG Method Application for Solving Gas Dynamics Problems;Advances in Theory and Practice of Computational Mechanics;2022

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