Theoretical analysis of linked leading-edge and trailing-edge flap-type controls at supersonic speeds / E. Carson Yates, Jr.
The use of linked leading-edge and trailing-edge flap-type controls for the purpose of reducing hinge moments at supersonic speeds has been analytically investigated. A series of linked controls with supersonic leading and trailing edges on swept and unswept wings has been studied for Mach numbers o...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1956.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3617. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3617
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| Y 3.N 21/5:6/3617 | Available Place a Hold |