UNT Libraries Government Documents Department - 2 Matching Results
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- Determination of General Relations for the Behavior of Turbulent Boundary Layers
- Report presenting an analysis of data for turbulent boundary layers along wings and bodies of various shapes in order to determine the fundamental variables that control the development of turbulent boundary layers. Results indicate that the type of velocity distribution in the boundary layer could be expressed in terms of a single parameter.
- Notes on the Effect of Surface Distortions on the Drag and Critical Mach Number of Airfoils
- "The effect of two-dimensional bumps and surface waviness on the pressure distribution over airfoils is considered. It is shown that the results of the analysis may be useful in evaluating the effects of accidental or intended surface distortions on the drag and critical Mach number of airfoils" (p. 1).