USAF/RAAF F-111 Flight Test with Active Separation Control-Reference-Cited by-同舟云学术

USAF/RAAF F-111 Flight Test with Active Separation Control

Published:2003-01-06 Issue: Volume: Page:
ISSN:
Container-title:41st Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Grove James¹,Shaw Leonard¹,Leugers John¹,Akroyd Graham²

Affiliation:

1. Air Force Research Laboratory

2. Royal Australian Air Force

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-9

Reference5 articles.

1. Clark, R. L., Evaluation of F-111 Weapon Bay Aero-Acoustic and Weapon Separation Improvement Techniques, AFFDL-TR-79-3003, February1979.

2. Stanek, M. L., Sinha, N., Ahuja, V. and Birkbeck, R. M. "Acoustic-Compatible Active Flow Control For Optimal Weapon Separation", AIAA-99-1911.

3. (ZP is in feet full scale). Figure 7. ASC flight hardware installed in RAAF F-111G aircraft. Figure 8. RAAF F-111G aircraft. Figure 9. Mach 0.95 forward separation, CTS vs. flight data. Figure 11. Mach 1.3 forward separation, CTS vs. flight data. Figure 13. Spectra on Aft Wall (MIC 9) for Each of the Mach Numbers Flown Figure 14. Acoustic Suppression Versus Frequency MACH0.80-20K MACH0.95-20K MACH1.10-30K MACH1.30-30K

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