Mach Number Effect on Supersonic Drag Reduction using Repetitive Laser Energy Depositions over a Blunt Body-Reference-Cited by-同舟云学术

Mach Number Effect on Supersonic Drag Reduction using Repetitive Laser Energy Depositions over a Blunt Body

Published:2017 Issue:5 Volume:60 Page:303-311
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

IWAKAWA Akira¹,SHODA Tatsuro¹,MAJIMA Ryosuke¹²,PHAM Son Hoang¹,SASOH Akihiro¹

Affiliation:

1. Department of Aerospace Engineering, Nagoya University

2. Currently, Aero-Engine, Space and Defense Business Area, IHI Corporation

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/60/5/60_T-16-34/_pdf

Reference32 articles.

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2. 2) Knight, D. D.: Survey of Aerodynamic Drag Reduction at High Speed by Energy Deposition, J. Propul. Power, 24 (2008), pp. 1153–1167.

3. 3) Georgievskii, P. and Levin, V.: Supersound Body Bypass with External Resources of Heat Release, Pisma v Zhurnal Tekhnicheskoi Fiz., 14 (1988), pp. 684–687.

4. 4) Tret’yakov, P. K. and Garanin, A. F.: Control of Supersonic Flow around Bodies by Means of High-Power Recurrent Optical Breakdown, Physics-Doklay, 41 (1996), pp. 566–597.

5. 5) Erdem, E., Kontis, K., and Yang, L.: Steady Energy Deposition at Mach 5 for Drag Reduction, Shock Waves, 22 (2012), pp. 285–298.

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