Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tips. : Subsonic leading edges / Kenneth Margolis.
On the basis of linearized-supersonic-flow theory, equations are derived for the lateral force and yawing moment due to combined angle of attack and rolling for families of thin sweptback tapered wings with streamwise tips. Results of the analysis are presented in the form of design charts which per...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1950.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2122. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2122
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| Y 3.N 21/5:6/2122 | Available Place a Hold |