Wind-tunnel investigation of ailerons on a low-drag airfoil. : 2 - The effect of thickened and beveled trailing edges / by Robert M. Crane and Ralph W. Holtzclaw.
An investigation was made in the Ames Aeronautical Laboratory 7- by 10-foot wind tunnel of the effects of a trailing edge of a 0.20-chord plain sealed aileron on an NACA 66,2-216 (a = 0.6) airfoil.
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| Other title: | NACA Wartime Reports. Series A. Technical report archive and image library. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1944]
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| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. A54. |
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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/A54
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| Y 3.N 21/5:11/A54 | Available Place a Hold |