A description is presented of a systematic procedure for obtaining generalized aerodynamic forces from the lifting-surface theory by the supersonic kernel-function method and for using those forces thus obtained in a Galerkin modal flutter analysis. The method is applicable to planforms with subsonic leading and supersonic trailing edges. Analytical flutter results were obtained and compared with experimental values from three flutter models.National Aeronautics and Space Act of 1958 NASA SCIENTIFIC AND TECHNICAL PUBLICATIONS Details on the ... 1 5 Ap ainl) xJO Not Retuii TECHNICAL REPORTS: Scientific and technical information considered important, complete, and aanbsp;...
|Title||:||Application of a supersonic kernel-function procedure to flutter analysis of thin lifting surfaces|
|Author||:||Herbert J. Cunningham, United States. National Aeronautics and Space Administration, Langley Research Center|