Laminar boundary layer at an infinite swept stagnation line with large rates of injection
- 1 October 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (10) , 1846-1851
- https://doi.org/10.2514/3.5999
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- On Laminar Boundary Layer BlowoffSIAM Journal on Applied Mathematics, 1970
- Boundary-layer flows with large injection and heat transfer.AIAA Journal, 1968
- Remarks on quasilinearization applied in boundary-layer calculations.AIAA Journal, 1966
- Application of quasilinearization to boundary- layer equationsAIAA Journal, 1964
- Helium Injection Into the Boundary Layer at an Axisymmetric Stagnation PointJournal of the Aerospace Sciences, 1962
- 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