Calculation of the three-dimensional flow field in supersonic inlets at angle of attack using a bicharacteristic method with discrete shock wave fitting
- 15 January 1979
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- A Second-Order Numerical Method of Characteristics for Three-Dimensional Supersonic Flow. Volume 1. Theoretical Development and ResultsPublished by Defense Technical Information Center (DTIC) ,1969
- The numerical solution of hyperbolic systems of partial differential equations in three independent variablesProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1960
- ber die partiellen Differenzengleichungen der mathematischen PhysikMathematische Annalen, 1928