Effect of boundary-layer transition on dynamic stability.
- 1 January 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 3 (1) , 46-52
- https://doi.org/10.2514/3.28384
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Boundary-Layer Transition at Supersonic Speeds - Three-Dimensional Roughness Effects (Spheres)Journal of the Aerospace Sciences, 1962
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952
- Turbulent Boundary Layer on a Cone in a Supersonic Flow at Zero Angle of AttackJournal of the Aeronautical Sciences, 1952
- Interrelationship Between Boundary Layer and Base PressureJournal of the Aeronautical Sciences, 1951