Transition of shock reflection at higher enthalpies for Earth and Mars atmospheres-Reference-Cited by-同舟云学术

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Transition of shock reflection at higher enthalpies for Earth and Mars atmospheres

Published:2021-11 Issue: Volume:188 Page:289-294
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Das Dipankar,Desai Siddesh,Kulkarni Vinayak^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

1. Hypersonic drag reduction mechanism of a novel combinational spike and multi-opposing jets aerodynamic configuration;Huang;Acta Astronaut.,2020

2. Spike root oblique jet effect on drag and heat load reduction performance for hypersonic vehicles;Ma;Acta Astronaut.,2020

3. Shock Wave Reflection Phenomena;Ben-Dor,1991

4. Transition from regular to Mach reflection of shock waves Part 2. The steady-flow criterion;Hornung;J. Fluid Mech.,1982

5. Reconsideration of oblique shock wave reflections in steady flows. Part 1. Experimental investigation;Chpoun;J. Fluid Mech.,1995

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