A simplified method for calculating aeroelastic effects on the roll of aircraft /
An approximate linearized lifting-surface theory is used in conjunction with structural influence coefficients to formulate a method for analyzing the aeroelastic behavior in roll of an aircraft. Rolling effectiveness and aileron-reversal speed are computed by the use of a Galerkin-type procedure. R...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, [D.C.] :
NACA,
1955
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3370 |
| Subjects: |
Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Stanford University
| Call Number: |
NACA TN 3370 |
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