Theoretical supersonic characteristics of inboard trailing-edge flaps having arbitrary sweep and taper. : Mach lines behnid flap leading and trailing edges / Julian H. Kainer and Jack E. Marte.
Generalized expressions in closed form have obtained by means of linearized theory for the aerodynamic characteristics (lift-, rolling-moment-, pitching-moment-, and hinge-moment-coefficient derivatives) due to deflection of inboard trailing-edge flaps. The analysis considers the effects of Mach num...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1950.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2205. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2205
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| Y 3.N 21/5:6/2205 | Available Place a Hold |