Some Examples of Laminar Boundary-Layer Flow on Rotating Blades
- 1 November 1956
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 23 (11) , 991-996
- https://doi.org/10.2514/8.3710
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- An Experimental Study of the One-Dimensional Refraction of a Rarefaction Wave at a Contact SurfaceJournal of the Aeronautical Sciences, 1956
- A Theoretical and Experimental Study of Shock-Tube FlowsJournal of the Aeronautical Sciences, 1955
- Three-Dimensional Laminar Boundary Layer with Small Cross-FlowJournal of the Aeronautical Sciences, 1954
- DENSITY MEASUREMENT IN SHOCK TUBE FLOW WITH THE CHRONO-INTERFEROMETERPublished by Defense Technical Information Center (DTIC) ,1954
- Simplified Laminar Boundary-Layer Calculations for Bodies of Revolution and Yawed WingsJournal of the Aeronautical Sciences, 1952
- The Laminar Boundary Layer on a Rotating BladeJournal of the Aeronautical Sciences, 1951
- The boundary layer of a class of infinite yawed cylindersMathematical Proceedings of the Cambridge Philosophical Society, 1950
- Potential Flow Around a Rotating Cylindrical BladeJournal of the Aeronautical Sciences, 1950
- The Boundary Layer of Yawed CylindersJournal of the Aeronautical Sciences, 1948