Experimental Investigation Of The Effects Of A Diffusion Field On A Laminar Boundary Layer In Supersonic Flow
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Analytical Investigation of the Effects of a Diffusion Field on a Laminar Boundary Layer in Supersonic Flow
Author | : John Russell Radbill |
Publisher | : |
Total Pages | : 216 |
Release | : 1958 |
Genre | : Aerodynamic heating |
ISBN | : |
An Experimental Investigation of the Effect of Surface Heating on Boundary-layer Transition on a Flat Plate in Supersonic Flow
Author | : Robert W. Higgins |
Publisher | : |
Total Pages | : 38 |
Release | : 1951 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Boundary-layer transition has been studied on a heated flat plate in an air stream at a Mach number of 2.40 and a length Reynolds number range from 475,000 to 3,930,000. The transition region was investigated at nominal plate temperature levels of 60, 100, 140, 180, and 260 degrees F and depicted in a series of curves of transition Reynolds numbers, based on boundary-layer dimensions and fluid properties evaluated alternatively at free-stream and wall temperatures. The average skin-friction coefficient over the laminar portion of the boundary layer was determined.
Index of NACA Technical Publications
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 498 |
Release | : 1952 |
Genre | : Aeronautics |
ISBN | : |