Calculation Method for Three-Dimensional Rotationally Symmetrical Laminar Boundary Layers with Arbitrary Free-Stream Velocity and Arbitrary Wall-Temperature Variation
- 1 May 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (5) , 309-316
- https://doi.org/10.2514/8.2633
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Heat Transfer to Constant-Property Laminar Boundary-Layer Flows with Power-Function Free-Stream Velocity and Wall-Temperature VariationJournal of the Aeronautical Sciences, 1952
- Calculating the response of an oscillator to arbitrary ground motion*Bulletin of the Seismological Society of America, 1941
- Some Aspects of Non-Stationary Airfoil Theory and Its Practical ApplicationJournal of the Aeronautical Sciences, 1941
- Der Einfluß großer Zähigkeit bei der Strömung um den Zylinder und um die KugelZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1936