Boundary layer over a slender parabola of revolution with fluid injection.
- 1 November 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (11) , 2040-2041
- https://doi.org/10.2514/3.3838
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- The Transverse Curvature Effect in Compressible Axially Symmetric Laminar Boundary-Layer FlowJournal of the Aeronautical Sciences, 1956
- The asymptotic boundary layer on a circular cylinder in axial incompressible flowQuarterly of Applied Mathematics, 1955