Unsteady two-dimensional subsonic transonic, and supersonic flow calculations by the method of characteristics

Author:

Chu Chong-Wei,Nadir Stefan

Publisher

Springer Berlin Heidelberg

Reference11 articles.

1. Magnus, R. J. and Yoshihara, H., “Calculations of Transonic Flow over an Oscillating Airfoil,” AIAA Paper 75-98, Presented at the AIAA 13th Aerospace Sciences Meeting, Pasadena, California, 1975.

2. Chu, C. W., “Compatibility Relations and a Generalized Finite-Difference Approximation for Three-Dimensional Steady Supersonic Flow,” AIAA Journal, Vol. 5, No. 3, March 1967, pp. 493–501.

3. Chu, C. W. and Powers, S. A., “Determination of Space Shuttle Flow Field by the Three-Dimensional Method of Characteristics,” NASA TMX-2506, February 1972, pp. 47–63.

4. Chu, C. W., “A New Algorithm for Three-Dimensional Method of Characteristics,” AIAA Journal, Vol, 10, No. 11 November 1972, pp. 1548–1550.

5. Chu, C. W., “Calculation of Three-Dimensional Supersonic Flow Fields about Aircraft Fuselages and Wings at General Angle of Attack,” NOR 72-182, March 1973, Northrop Corporation, Hawthorne, California.

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