Effects of leading-edge radius and maximum thickness-chord ratio on the variation with Mach number of the aerodynamic characteristics of several thin NACA airfoil sections / Robert E. Berggren and Donald J. Graham.
A wind-tunnel investigation has been made to determine the effects of leading-edge radius and maximum thickness-chord ratio on the variation with Mach number of the aerodynamic characteristics of several thin symmetrical NACA 4-digit-series airfoil sections. The Mach number range of the investigatio...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1954.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3172. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3172
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| Y 3.N 21/5:6/3172 | Available Place a Hold |