Theoretical analyses to determine unbalanced trailing-edge controls having minimum hinge moments due to deflection at supersonic speeds / Kennith L. Goin.
Analyses based on theoretical results of NACA Report 1041 have been made to determine the plan forms of unbalanced trailing-edge flap-type controls having minimum hinge moments due to deflection and requiring minimum work to overcome the hinge moments due to deflection at supersonic speeds. Ratios o...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1955.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3471. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3471
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| Y 3.N 21/5:6/3471 | Available Place a Hold |