Investigation of the boundary layer about a symmetrical airfoil in a wind tunnel of low turbulence / by Albert E. von Doenhoff.
An extensive series of boundary-layer surveys was made over the surface of an NACA 0012 airfoil at zero lift. The surveys were made at Reynolds numbers, based on the chord, of 2,675,000, 3,780,000, 5,350,000, and 7,550,000. The drag of the airfoil was measured by the wake-survey method throughout a...
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| Main Author: | |
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| Corporate Authors: | , |
| Other title: | NACA Wartime Reports. Series L. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1940]
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| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L507. |
| Subjects: |
Norlin Library - Basement - Government Information - US
| Call Number: |
Y 3.N 21/5:11/L507
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| Y 3.N 21/5:11/L507 | Available Place a Hold |