Wind-tunnel investigation of an NACA 23012 airfoil with a 0.30-airfoil-chord double slotted flap / by Paul E. Purser, Jack Fischel, and John M. Riebe.
Tests to determine the effect of flap position and deflection on the aerodynamic characteristics of an NACA 23012 airfoil with a double slotted flap having a chord 30 percent of the airfoil chord (0.30c) were conducted in the LMAL 7- by 10-foot tunnel. In addition, a few tests were made to determine...
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| Main Author: | |
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| Corporate Authors: | , |
| Other Authors: | , |
| Other title: | NACA Wartime Reports. Series L. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1942]
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| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L469. |
| Subjects: |
Norlin Library - Basement - Government Information - US
| Call Number: |
Y 3.N 21/5:11/L469
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| Y 3.N 21/5:11/L469 | Available Place a Hold |