External burning assisted projectile - Theory and experiment
Author:
Affiliation:
1. U.S. Naval Postgraduate School, Monterey, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1973-1193
Reference16 articles.
1. 51. C. Stiahls, "Theoretical Consideration of Combustion Effects on Ease Pressure in Suversonic Flight," hielfthSyrDosiumCornbustion, Combustion Institute, Pittsburgh, PA., pp.1163-1171. 1969.
2. D. D. Davis, "E,xtension of Simplifisd Mxing Theory to Axially Symmetric Supersonic Wake Flows and Application to Base Pressure Problem for a Body of Revolutinn," Princeton Univsrsitx M.Sc. Thesis, 24-V-1952.
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