Laminar boundary layer on a cone at incidence in supersonic flow
- 19 January 1970
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- An experimental study of a yawed circular cone in hypersonic flowsAIAA Journal, 1969
- Application of the method of nonlinear simultaneous displacements togeneral three- dimensional stagnation point boundary layer equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- INVISCID FLOW FIELD PAST A POINTED CONE AT AN ANGLE OF ATTACK. PART 1 - ANALYSISPublished by Defense Technical Information Center (DTIC) ,1965
- AN INTEGRAL METHOD FOR CALCULATION OF SUPERSONIC LAMINAR BOUNDARY LAYER WITH HEAT TRANSFER ON YAWED CONEAIAA Journal, 1963
- Supersonic flow past cones of general cross-sectionJournal of Fluid Mechanics, 1962
- Laminar Heat Transfer on Three-Dimensional Blunt Nosed Bodies in Hypersonic FlowARS Journal, 1959
- On Supersonic Flow Past a Slightly Yawing Cone IIJournal of Mathematics and Physics, 1951
- A Variational Principle for Plastic Materials with Strain-HardeningJournal of Mathematics and Physics, 1948