Computational and experimental investigation of F/A-18E sting support and afterbody distortion effects
Author:
Affiliation:
1. McDonnell Douglas Corporation, St. Louis, Missouri 63166-0516
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46953
Reference5 articles.
1. filler, M. A. *'Sting Distortion and Jet Effects Test of a 15-Percent Scale F-18E/F Model at Subsonic and Transonic Mach Numbers," Arnold Engineering and Development Center TSR-94-P10, Oct. 1994.
2. A three dimensional zonal Navier-Stokes code for subsonic through hypersonic propulsion flowfields
3. A critical evaluation of CFD predictions of full aircraft drag increments
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