Velocity profile model for two-dimensional zero-pressure gradient transitional boundary layers
- 1 August 1989
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 27 (8) , 1127-1132
- https://doi.org/10.2514/3.10233
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Observations of supersonic free shear layersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- A Theoretical and Experimental Investigation of the Constant Area, Supersonic-Supersonic EjectorAIAA Journal, 1982
- Influence of the Pressure Gradient on the Law of the WallAIAA Journal, 1982
- Compound-Compressible Nozzle FlowJournal of Applied Mechanics, 1967
- Ein Differenzenverfahren zur Lösung der Grenzschichtgleichung für stationäre, laminare, inkompressible StrömungArchive of Applied Mechanics, 1964
- The law of the wake in the turbulent boundary layerJournal of Fluid Mechanics, 1956
- The calculation of the viscous drag of bodies of revolution / by Paul S. Granville.Published by Biodiversity Heritage Library ,1953
- Zur näherungsweisen Integration der Differentialgleichung der Iaminaren GrenzschichtZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1921