Comparison of Analytical and Experimental Supersonic Aerodynamic Characteristics of a Forward Control Missile
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.62226
Reference4 articles.
1. Experimental and analytical comparison of aerodynamic characteristics of a forward-control missile
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1. Numerical Investigation of Canard-Controlled Missile with Planar and Grid Fins;Journal of Spacecraft and Rockets;2003-05
2. Subsonic Flow CFD Investigation of Canard-Controlled Missile with Planar and Grid Fins;41st Aerospace Sciences Meeting and Exhibit;2003-01-06
3. CFD Investigation of Canard-Controlled Missile with Planar and Grid Fins in Supersonic Flow;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2002-06-25
4. Experimental study of tail-span effects on a canard-controlled missile;Journal of Spacecraft and Rockets;1993-09
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