The Homogeneous Boundary Layer at an Axisymmetric Stagnation Point With Large Rates of Injection
- 1 January 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (1) , 48-60
- https://doi.org/10.2514/8.9302
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- The Effect of Helium Injection at an Axially Symmetric Stagnation PointJournal of the Aerospace Sciences, 1959
- Laminar Heat-Transfer and Pressure Measurements Over Blunt-Nosed Cones at Large Angle of AttackJournal of the Aerospace Sciences, 1958
- On Heat Transfer over a Sweat-Cooled Surface in Laminar Compressible Flow with a Pressure GradientJournal of the Aeronautical Sciences, 1952
- A process for the step-by-step integration of differential equations in an automatic digital computing machineMathematical Proceedings of the Cambridge Philosophical Society, 1951