Wind-Tunnel Tests of an Aircraft Turret Model-Reference-Cited by-同舟云学术

Wind-Tunnel Tests of an Aircraft Turret Model

Published:2000-05 Issue:3 Volume:37 Page:368-376
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Snyder C. H.¹,Franke M. E.¹,Masquelier M. L.²

Affiliation:

1. Air Force Institute of Technology, Wright–Patterson Air Force Base, Ohio 45433

2. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.2625

Reference10 articles.

1. Mullane, R. M. “An Experimental Investigation of Methodsof Suppressing the Unsteady Torque Exerted on the Upper Turning Mirror of an Aircraft Mounted Coelostat Turret,” M.S. Thesis, AFIT/GAE/AE/75J-6,Dept. of AeroMechanical Engineering, Air Force Inst. of Technology, Wright-Patterson AFB, OH, June 1975.

2. 4King, B. W. “Fluctuating Wind Forces Measured on a Bluff Body Extending from a Cavity,” M.S. Thesis, AFIT/GAE/ENY/89D-19,Dept. of Aeronautics and Astronautics, Air Force Inst. of Technology, Wright-Patterson AFB, OH, Dec. 1989.

3. 5Snyder, C. H. “Wind Tunnel Testing for Drag Reduction of an Aircraft Laser Turret,” M.S. Thesis, AFIT/GAE/ENY/98J-02,Dept. of Aeronautics and Astronautics, Air Force Inst. of Technology, Wright-Patterson AFB, OH, June 1998.

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