Flow Computations in Inlets at Incidence Using a Shock Fitting Bicharacteristic Method

This publication has 6 references indexed in Scilit:

• Characteristics procedure for supersonic flows including consideration of viscous contributions to flow rotationality
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1976
• Shock Fitting Method for Complicated Two-Dimensional Supersonic Flows
  AIAA Journal, 1976
• Internal flow calculations for axisymmetric supersonic inlets at angle of attack
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1975
• A Second-Order Numerical Method of Characteristics for Three-Dimensional Supersonic Flow. Volume 1. Theoretical Development and Results
  Published by Defense Technical Information Center (DTIC) ,1969
• The numerical solution of hyperbolic systems of partial differential equations in three independent variables
  Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1960
• ber die partiellen Differenzengleichungen der mathematischen Physik
  Mathematische Annalen, 1928