On the PLK Method and the Supersonic Blunt-Body Problem
Author:
Affiliation:
1. Polytechnic Institute of Brooklyn,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.9363
Reference27 articles.
1. E2= - [(1 - 8)/28]{P/f)fT(43j)
2. with c = 1 + [(1 - 8)/MJ8] (44a)
3. a2=[(T+i)/2]c8 - [(Y - l)/2]W2(44b) f(ry2) = P i j - U + a / U - O = [(1 - 5 ) / ( l + 8)] X
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2. Parameters determining the shape of the subsonic section of a shock wave in the case of axisymmetric flow;Fluid Dynamics;1977
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4. The supersonic flow round blunt bodies of revolution with a break in the generator;USSR Computational Mathematics and Mathematical Physics;1966-01
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