Aerothermodynamic effects of controlled heat release within the hypersonic shock layer around a large angle blunt cone-Reference-Cited by-同舟云学术

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Aerothermodynamic effects of controlled heat release within the hypersonic shock layer around a large angle blunt cone

Published:2018-10 Issue:10 Volume:30 Page:106103
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Deep Sneh¹,Jagadeesh G.¹

Affiliation:

1. Department of Aerospace Engineering, Indian Institute of Science, Bangalore 560012, India

Funder

Defence Research and Development Organisation

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Link

http://aip.scitation.org/doi/pdf/10.1063/1.5046191

Reference49 articles.

1. J. D. Anderson, Jr. Hypersonic and High Temperature Gas Dynamics (AIAA Publications, Reston, VA, 2000), pp. 321–332.

2. Axisymmetric hypersonic flow with strong viscous interaction

3. Hypersonic flow over axially symmetric spiked bodies

4. Preliminary Investigations of Spiked Bodies at Hypersonic Speeds

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