Universal scaling parameter for a counter jet drag reduction technique in supersonic flows-Reference-Cited by-同舟云学术

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Universal scaling parameter for a counter jet drag reduction technique in supersonic flows

Published:2020-03-01 Issue:3 Volume:32 Page:036105
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Desai Siddesh¹²^ORCID,Prakash K Vishnu²,Kulkarni Vinayak²,Gadgil Hrishikesh³

Affiliation:

1. Department of Computational Science, Kobe University, Kobe 6578501, Japan

2. Department of Mechanical Engineering, Indian Institute of Technology Guwahati, Guwahati 781039, India

3. Department of Aerospace Engineering, Indian Institute of Technology Bombay, Mumbai 400076, India

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/10.1063/1.5140029

Reference37 articles.

1. Moderation of near-field pressure over a supersonic flight model using laser-pulse energy deposition

2. A theoretical approximation of the shock standoff distance for supersonic flows around a circular cylinder

3. Investigation of unsteady, hypersonic, laminar separated flows over a double cone geometry using a kinetic approach

4. Hypersonic aerodynamic heating over a flared cone with wavy wall

5. Experimental study of forward-facing cavity with energy deposition in hypersonic flow conditions

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