Numerical simulation of high-incidence flow over the F-18 fuselage forebody
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46072
Reference32 articles.
1. Navier-Stokes solutions about the F/A-18 forebody-LEX configuration
2. Numerical simulation of vortical flow over an elliptical-body missile at high angles of attack
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