Approximate inviscid, nonadiabatic stagnation region flow field solution
Author:
Affiliation:
1. North American Aviation, Inc., Downey, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3196
Reference12 articles.
1. Alden, H. L., Habert, R. H., and Hill, J. A. F. "Gasdynamics of high-altitude rocket plumes/7MITHRAS Inc.,Semiannual Technical Report (December 31, 1963)
2. also Hill,J. A. F.and Habert, R. H. "Gasdynamics of high-altitude missile trails," MITHRAS Inc., Rept.MC-61-18-R1 (1963).
3. Table of the zeros of the Legendre polynomials of order 1-16 and the weight coefficients for Gauss’ mechanical quadrature formula
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