Effect of sidewall leading edge sweep direction on performance of a hypersonic 3-D inlet-Reference-Cited by-同舟云学术

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Effect of sidewall leading edge sweep direction on performance of a hypersonic 3-D inlet

Published:2000-07-24 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Ye Fangrong¹,Huque Ziaul¹,Butuk Nelson¹

Affiliation:

1. Prairie View A & M Univ., TX

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3600

Reference19 articles.

1. Layer Interaction,"AFFDL-TR-65-36,

2. AFFDL-TR-65-36,GECo.,Evendale,OH,

3. LJ."The Effects of Propilsion System-Airframe Interactionsonthe Performance of HypersonicAircraft". AIAA-67-493, 1967.

4. Studies of Engine-Airframe Integration on Hypersonic Aircraft

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