Computational Simulation Improvements of Supersonic High-Angle-of-Attack Missile Flows
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433-7913
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3433
Reference19 articles.
1. Computation of turbulent supersonic flows around pointed bodies having crossflow separation
2. Calculations and comparisons of the flowfield about an ogive cylinder at M = 3.5
3. Navier-Stokes simulations of slender axisymmetric shapes in supersonic, turbulent flow
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