Aerothermodynamic Assessment of Spiked Configuration for Drag Reduction at Hypersonic Speeds-Reference-Cited by-同舟云学术

Aerothermodynamic Assessment of Spiked Configuration for Drag Reduction at Hypersonic Speeds

Published:2020-11 Issue:6 Volume:33 Page:04020076
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Kumar Shailendra¹,Kulkarni Vinayak²^ORCID,Jammy Satya Pramod³

Affiliation:

1. Research Scholar, Dept. of Mechanical Engineering, Indian Institute of Technology Guwahati, Guwahati 781039, India.

2. Associate Professor, Dept. of Mechanical Engineering, Indian Institute of Technology Guwahati, Guwahati 781039, India (corresponding author). ORCID: .

3. Assistant Professor, Dept. of Mechanical Engineering, Sri Ramaswamy Memorial Univ. AP, Amaravati, Andhra Pradesh 522502, India.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001180

Reference29 articles.

1. Recent advances in the aerothermodynamics of spiked hypersonic vehicles;Ahmed M. Y.;Int. J. Heat Mass Transfer,2011

2. Shock-wave shapes around spherical-and cylindrical-nosed bodies.

3. Delusive Influence of Nondimensional Numbers in Canonical Hypersonic Nonequilibrium Flows

4. Drag reduction on a spiked body at hypersonic speed

5. Concentrated energy addition for active drag reduction in hypersonic flow regime

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