Numerical study on performance of supersonic inlets with various three-dimensional bumps-Reference-Cited by-同舟云学术

Numerical study on performance of supersonic inlets with various three-dimensional bumps

Published:2008-08 Issue:8 Volume:22 Page:1640-1647
ISSN:1738-494X
Container-title:Journal of Mechanical Science and Technology
language:en
Short-container-title:J Mech Sci Technol

Author:

Kim Sang Dug,Song Dong Joo

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Link

http://link.springer.com/content/pdf/10.1007/s12206-008-0503-9.pdf

Reference12 articles.

1. M. C. Gridley and S. H. Walker, Advanced Aero-Engine Concepts and Controls, AGARD Conf. Proc. 572, 86th Symposium, Seattle, WA, USA, (1996).

2. J. Seddon and E. L. Goldsmith, Intake Aerodynamics, Blackwell Science Ltd, (1999).

3. J. Benson and L. D. Miller, Mach 5 Turbo-Ramjet Inlet Design and Performance, ISABE 91-7079, ISABE Conference, Nottingham, U.K., 12 (1991) 746–753.

4. J. Anderson, Airframe/Propulsion Integration of Supersonic Vehicles, 26th AIAA/SAE/ ASME/ASEE Joint Proportion Conference, AIAA 90-2151, Orlando, Fl, USA, (1990).

5. P. C. Simon, D. W. Brown and R. G. Huff, Performance of External-Compression Bump Inlet at Mach Number of 1.5 to 2.0, NACA-RM-E56L19, National Advisory Committee for Aeronautics, Washington, USA (1957).

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