TECHNICAL PAPERS: Gas Turbines: Aircraft Engine

Demonstration of Fluidic Throat Skewing for Thrust Vectoring in Structurally Fixed Nozzles

[+] Author and Article Information
P. J. Yagle, D. N. Miller, K. B. Ginn, J. W. Hamstra

Lockheed Martin Aeronautics Company, P.O. Box 748, MZ 9333, Fort Worth, TX 76101

J. Eng. Gas Turbines Power 123(3), 502-507 (Jan 01, 2001) (6 pages) doi:10.1115/1.1361109 History: Received February 01, 2000; Revised January 01, 2001
Copyright © 2001 by ASME
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Miller, D. N., Yagle, P. J., and Hamstra, J. W., 1999, “Fluidic Throat Skewing for Thrust Vectoring in Fixed Geometry Nozzles,” AIAA 99-0365.
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Grahic Jump Location
Characteristics of shock vector control and fluidic throat skewing for jet flow control
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Initial and final state for time-accurate CFD calculations
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Time response of thrust vector angle
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LMTAS thrust measurement facility
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Conformal fluidic nozzle internal flowpath geometry
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Conformal fluidic nozzle model
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Multiaxis vectoring performance
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Comparison of thrust vectoring methods
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Comparison of fluidic throat skewing and shock vector control



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