Inviscid transonic flow field analysis

Author:

Lin T. C.,Zhenxue Jia

Publisher

Springer Science and Business Media LLC

Reference102 articles.

1. Aungier RH 1970 A computational method for exact, direct and unified solutions for axisymmetric flow over blunt bodies of arbitrary shape, AFWL-TR-70-16

2. Back L H, Massier P H & Gier H L 1965AIAAJ. 3 1606

3. Back L H & Cuffel R F 1971J. Spacecraft. 8 196

4. Barwell R W & Davis R M 1971 A computer program for calculating inviscid adiabatic flow about blunt bodies travelling at supersonic and hypersonic speeds at angle of attack, NASA TM X-2334.

5. Bauer F, Garabedian P R & Korn D 1975Supercritical wing § 2 Lecture notes in economics and mathematical systems (New York: Springer Verlag)

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