Boundary-layer flows with large injection and heat transfer.
- 1 January 1968
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (1), 22-28
- https://doi.org/10.2514/3.4436
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Remarks on quasilinearization applied in boundary-layer calculations.AIAA Journal, 1966
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964
- Application of quasilinearization to boundary- layer equationsAIAA Journal, 1964
- The Homogeneous Boundary Layer at an Axisymmetric Stagnation Point With Large Rates of InjectionJournal of the Aerospace Sciences, 1962
- Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight SpeedsJournal of Jet Propulsion, 1956
- Grenzen der GrenzschichtbeeinflussungZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1944