Effect of Fuselage Cross Section on Aerodynamic Characteristics of Reusable Launch Vehicles

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ISSN Print: 2165-3852
ISSN Online: 2165-3860
www.scirp.org/journal/ojfd
E-mail: ojfd@scirp.org

"Effect of Fuselage Cross Section on Aerodynamic Characteristics of Reusable Launch Vehicles"
written by Kenji Tadakuma, Yasuhiro Tani, Shigeru Aso,
published by Open Journal of Fluid Dynamics, Vol.6 No.3, 2016

has been cited by the following article(s):

[1]	Shape Optimization of the Cross-Section for Noncircular Hypersonic Missile Forebody
	2020

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