Helium Injection Into the Boundary Layer at an Axisymmetric Stagnation Point
- 1 August 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (8) , 921-934
- https://doi.org/10.2514/8.9661
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- The Downstream Influence of Mass Transfer at the Nost of a Slender ConeJournal of the Aerospace Sciences, 1962
- The Homogeneous Boundary Layer at an Axisymmetric Stagnation Point With Large Rates of InjectionJournal of the Aerospace Sciences, 1962
- Theory of Mixing and Chemical Reaction in the Opposed-Jet Diffusion FlameARS Journal, 1961
- Experimental Investigation of the Downstream Influence of Stagnation-Point Mass TransferJournal of the Aerospace Sciences, 1961
- Dynamics of a dissociating gas Part I Equilibrium flowJournal of Fluid Mechanics, 1957