Laminar boundary layer and position of transition point were investigated on heated flat plate; it was found that Reynolds number of transition decreases as temperature of plate is increased.
Investigations of effects of surface temperature and single roughness elements on boundary-layer transition
Nat Advisory Committee Aeronautics -- Tech Note
1947
17 pages
14 Supp Plates, Bibliography
Report
Englisch
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Boundary-layer transition at Mach 3.12 with and without single roughness elements
Engineering Index Backfile | 1954
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