A Numerical Study on Flow-Through Model Design Considering the Internal Loss-Reference-Cited by-同舟云学术

A Numerical Study on Flow-Through Model Design Considering the Internal Loss

Published:2019-06-17 Issue:3 Volume:20 Page:688-696
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Lee Younghwan^ORCID

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

http://link.springer.com/content/pdf/10.1007/s42405-019-00186-1.pdf

Reference16 articles.

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2. Capone FJ, Bare EA, Hollenback D, Hutchison R (1984) Subsonic/supersonic aerodynamic characteristics for a tactical supercruiser. In: AIAA 2nd applied aerodynamics conference, AIAA-84-2192

3. Bowcutt B, Burrows R, Weir J (1999) Techniques to determine Fasthawk missile aerodynamics including Inlet effects. In: 37th AIAA aerospace sciences meeting and exhibit, AIAA-99-0432, Reno, NV

4. Jung SY, Byon W (2010) Internal flow path design for supersonic flow-through model. KSAS Conf 4:2010

5. Giori BR (2013) Experimental and computational analysis of a miniature ramjet at Mach 4.0, Master’s Thesis, Naval Postgraduate School, Monterey, CA

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