Extension of the second order theory of entry mechanics to nearly exact solutions
Author:
Affiliation:
1. NORTH AMERICAN AVIATION, INC., SPACE AND INFORMATION SYSTEMS DIV., DOWNEY, CALIF.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1966-488
Reference13 articles.
1. Lah, W. H. T. "A Second Order Theory of Entry Mechanics into a Planetary Atmosphere." IAS Preprint 61-116-1810 (June 13. 19611;also J. Aerospace Sci. 29, 1210-1222(1962).
2. Allen, H. J. and Eggers, A. J., Jr. "A Study ofthe Motion and Aerodynamic Heating of Missiles Entering the Earth's Atmosphere at High Supersonic Speeds,' NACA TN 4047 (October 19571.
3. Egge=$, A. J., Jr., Allen, H. J., and Neice. S. E, "A Comparative Analysis of the Performnce d Long Range Hypervelocity Vehicles," NACA TN 4046 (October 19571.
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1. Entry Mechanics and Dynamics;Re-entry and Planetary Entry Physics and Technology;1968
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