Shock-fitting bicharacteristic algorithm for three-dimensional scarfed nozzle flowfields
Author:
Affiliation:
1. Purdue University, West Lafayette, Indiana
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8023
Reference9 articles.
1. 2Buchman, J. J. and Sternfeld, A. S. "Analysis of Problems Related to Thrust Reversal in Solid Propellant Motors," AIAA Paper 72-1110,1972.
2. A Second-Order Numerical Method of Characteristics for Three-Dimensional Supersonic Flow. Volume 1. Theoretical Development and Results
3. 5Dash, S. M. and DelGuidice, P. D. "Analysis of Three-Dimensional Ducted and Exhaust Plume Flowfields,'M/y4,4 Journal, Vol.16, Aug. 1978, pp.823-830.
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