Analysis of Embedded Shock Waves Calculated by Relaxation Methods
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49309
Reference13 articles.
1. Calculation of plane steady transonic flows
2. Dr. E. Kreyßig (Prof. a. d. Univ. Ottawa, Kanada), Differentialgeometrie (Mathematik und ihre Anwendung in Physik und Technik, Reihe A, Band 25). XII + 421 S. m. 105 Abb. Leipzig 1957. Akademische Verlagsgesellschaft Geest & Portig K. G. Preis geb. 36,— DM
3. Solution of the transonic potential equation using a mixed finite difference system
4. Krupp, J. A. "The Numerical Calculation of Plane Steady Transonic Flow Past Thin Lifting Airfoils," Ph.D. thesis,June 1971, Univ. of Washington, Seattle, Wash.
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