Numerical simulation of HSCT inlet operability with angle of attack-Reference-Cited by-同舟云学术

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Numerical simulation of HSCT inlet operability with angle of attack

Published:1997-07-06 Issue: Volume: Page:
ISSN:
Container-title:33rd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Zha Ge-Cheng¹,Knight Doyle¹,Smith Donald¹,Haas Martin²,Zha Ge-Cheng¹,Knight Doyle¹,Smith Donald¹,Haas Martin²

Affiliation:

1. Rutgers Univ., Piscataway, NJ

2. United Technologies Research Center, East Hartford, CT

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2761

Reference23 articles.

1. J. Saunders and T. Keith, "Results from Computational Analysis of a Mixed Compression Supersonic Inlet." AIAA Paper 91-2581,1991.

2. G. Cooper and J. Sirbaugh, "PARC Code: Theory and Usage." AEDC-TR-89-15,1989.

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