An Experimental Investigation Of The Effect Of Surface Heating On Boundary Layer Transition On A Flat Plate In Supersonic Flow
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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.
Author | : K. R. Czarnecki |
Publisher | : |
Total Pages | : 30 |
Release | : 1952 |
Genre | : Body of revolution |
ISBN | : |
Author | : Ivan E. Beckwith |
Publisher | : |
Total Pages | : 38 |
Release | : 1956 |
Genre | : |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 28 |
Release | : 1951 |
Genre | : Aerodynamics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 672 |
Release | : 1951 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 1004 |
Release | : 1970 |
Genre | : |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 462 |
Release | : 1954 |
Genre | : Aerodynamics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 1308 |
Release | : 1954 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 40 |
Release | : 1957 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 500 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |