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...
Main Author: | |
---|---|
Corporate Author: | |
Other Authors: | , |
Format: | Government Document Book |
Language: | English |
Published: |
Washington, [D.C.] :
NACA,
1955
|
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 |
---|