Proper Use of the M.I.T. Tables for Supersonic Flow Past Inclined Cones
Author:
Affiliation:
1. The RAND Corporation, Santa Monica, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.1957
Reference6 articles.
1. These forms of the continuity and dynamical equations are given by L. Hopf, Handbuch der Physik, Bd VII, Mechanik der fliissigen und gasformigen Korper, p.95.
2. The flow due to a rotating disc
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1. Calculation of hypersonic flow over bodies of revolution at small angles of attack;AIAA Journal;1965-03
2. A Guide to the Use of the M.I.T. Cone Tables;Journal of the Aeronautical Sciences;1954-05
3. Rocket Measurements of Upper Atmosphere Ambient Temperature and Pressure in the 30‐ to 75‐Kilometer Region;Journal of Applied Physics;1954-02
4. Parameters Predicting Failure of Partial Diagonal Tension Beams;Journal of the Aeronautical Sciences;1952-02
5. Supersonic Flow Around Cones at Large Yaw;Journal of the Aeronautical Sciences;1952-02
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