Separation Dynamics of Air-to-Air Missile Using a Grid-Free Euler Solver
Author:
Affiliation:
1. Defence Research and Development Laboratory, Kanchanbagh, Hyderabad, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031791
Reference24 articles.
1. ObermarkJ. “Verification of Simulation Results Using Scale Model Flight Test Trajectories,” U.S. Army Research, Development, and Engineering Command TR AMR-AE-04-01, Redstone Arsenal, AL, May 2004.
2. Recent developments in captive trajectory systems of the ONERA Modane wind tunnels
3. Simulations of Store Separation from an F/A-18 with a Cartesian Method
4. Applications of a highly efficient numerical method for overset-mesh moving body problems
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