Viscous effects above the wake shock wave in the laminar near wake
- 24 June 1968
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Experimental investigation of far wakes behind two-dimensional slender bodies at M sub infinity equals 6Published by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- An interaction model of a supersonic laminar boundary layer on sharpand rounded backward facing steps.AIAA Journal, 1968
- Upstream influence of the base pressure.AIAA Journal, 1968
- Experimental investigation of laminar near wakes behind 20 deg wedges at M infinity equals 6Published by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Near wake of a blunt body at hypersonic speedsAIAA Journal, 1965
- G. The Method of CharacteristicsPublished by Walter de Gruyter GmbH ,1954