Numerical Analysis of a Swept-Fin Missile
Author:
Affiliation:
1. U.S. Air Force Institute of Technology, Wright–Patterson Air Force Base, Ohio 45433-7765
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3203
Reference14 articles.
1. Aerodynamic test and analysis of a slender generic missile configuration
2. Navier-Stokes simulations of slender axisymmetric shapes in supersonic, turbulent flow
3. Moran, K. J. “An Aerodynamic and Static-Stability Analysis of the Hypersonic Applied Research Technology (HART) Missile,” Ph.D. Dissertation, Graduate School of Engineering,U.S.Air Force Inst. of Technology, Wright-Patterson AFB,OH, April 1994.
4. Experimental study of supersonic turbulent flow on a blunted axisymmetric body
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