Supersonic separated and reattaching laminar flows- i - general theory and application to adiabatic boundary layer-shock wave interactions
- 20 January 1964
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- The Effects of Heat Transfer on Laminar-Boundary-Layer Separation in Supersonic FlowAeronautical Quarterly, 1961
- A Theoretical Investigation of the Interaction Between Shock Waves and Boundary LayersJournal of the Aerospace Sciences, 1958
- Die Ablösungsbedingung von GrenzschichtenPublished by Springer Nature ,1958
- On the Boundary-Layer Equations in Hypersonic Flow and Their Approximate SolutionsJournal of the Aeronautical Sciences, 1953
- Simplified Laminar Boundary-Layer Calculations for Bodies of Revolution and Yawed WingsJournal of the Aeronautical Sciences, 1952
- Approximate Calculation of the Laminar Boundary LayerAeronautical Quarterly, 1949
- Anwendung des Energiesatzes von Wieghardt auf einparametrige Geschwindigkeitsprofile in laminaren GrenzschichtenArchive of Applied Mechanics, 1948
- CVI.An approximate solution of the boundary layer equations for a flat plateJournal of Computers in Education, 1937