Damping-in-roll calculations for slender swept-back wings and slender wing-body combinations / Harvard Lomax and Max A. Heaslet.
The damping-in-roll parameter is calculated theoretically for triangular wings on cylindrical bodies and for a class of wings with swept-back plan forms. The analysis is based on the usual assumptions of linearized compressible-flow theory together with the added restriction that at the free-stream...
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| Other title: | Technical report archive and image library. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1949.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1950. |
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Internet
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| Call Number: |
Y 3.N 21/5:6/1950
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| Y 3.N 21/5:6/1950 | Available Place a Hold |