Effects of compressibility on maximum lift coefficients for six propeller airfoils / by Harold E. Cleary.
An extension of previously reported data on the variation of lift coefficient with Mach number, camber, and thickness ratio is presented. The data were obtained from pressure-distribution tests in the Langley 8-foot high-speed tunnel of six propeller airfoils of 1-foot chord.
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| Corporate Authors: | , |
| Other title: | NACA Wartime Reports. Series L. Technical report archive and image library. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1945]
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| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L514. |
| Subjects: |
Internet
Search for the full-text version of this title in HathiTrustNorlin Library - Basement - Government Information - US
| Call Number: |
Y 3.N 21/5:11/L514
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| Y 3.N 21/5:11/L514 | Available Place a Hold |