论文信息 - NASA Technical Note D-6012 APPLICATION OF A SUPERSONIC KERNEL-FUNCTION PROCEDURE TO FLUTTER ANALYSIS OF THIN LIFTING SURFACES - 字舞流文

NASA Technical Note D-6012 APPLICATION OF A SUPERSONIC KERNEL-FUNCTION PROCEDURE TO FLUTTER ANALYSIS OF THIN LIFTING SURFACES

Flutter analysis for thin lifting surfaces by application of supersonic kernel function procedure

Herbert J. Cunningham

[1] G. M. Levey,et al. EXPERIMENTAL AND CALCULATED RESULTS OF A FLUTTER INVESTIGATION OF SOME VERY LOW ASPECT-RATIO FLAT-PLATE SURFACES AT MACH NUMBERS FROM 0.62 TO 3.00 , 1959 .

[2] Herbert J . Cunningham. Improved numerical procedure for harmonically deforming lifting surfaces from the supersonic kernel function method. , 1966 .

[3] J. G. F. Francis,et al. The QR Transformation A Unitary Analogue to the LR Transformation - Part 1 , 1961, Comput. J..

[4] H. J. Cunningham. Flutter Analysis of Flat Rectangular Panels Based on Three-Dimensional Supersonic Potential Flow , 1963 .