Spike-Nosed Projectiles with Vortex Rings: Steady and Nonsteady Flow Simulations
Author:
Affiliation:
1. U.S. Army Research Laboratory, Aberdeen Proving Ground, Maryland 21005-5066
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.55700
Reference11 articles.
1. Transonic flow modes of an axisymmetric blunt body
2. Flow Oscillations of Spike-Tipped Bodies
3. Modes of shock-wave oscillations on spike-tipped bodies
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