Computational Study of a High-Performance Submerged Inlet with Bleeding Vortex-Reference-Cited by-同舟云学术

Computational Study of a High-Performance Submerged Inlet with Bleeding Vortex

Published:2012-05 Issue:3 Volume:49 Page:852-860
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Cheng Dai-Shu¹,Tan Hui-Jun¹,Sun Shu¹,Tong Yue¹

Affiliation:

1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031483

Reference24 articles.

1. Numerical Analysis and Experimental Validation of a Submerged Inlet on the Plane Surface

2. Taskingoglu, E. "A Multiobjective Shape Optimization Study for a Subsonic Submerged Inlet," Ph.D. Dissertation,Rutgers Univ., Piscataway, NJ, May 2004.

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