A number of calculations of bending-torsion wing flutter are made at two Mach numbers, m=
0 (incompressible case) and m= 0.7, and results are compared. The air forces employed for …

IN analytical investigations of bending-torsion flutter of high-aspect ratio, straight wings, the
flutter speed increases sharply below a certain mass-density ratio ju. 1'2 This would prevent …

Part I. Possio's Derivative Theory for an Infinite Aerofoil Moving at Subsonic Speeds. The
derivative theory due to C. Possio for an infinite aerofoil moving at subsonic speeds is …

This report describes work which has been done to investigate the possibility that the flexure-
torsion flutter speed of a wing may be less at high incidences than at low incidences, and …

Flutter calculations for several swept and unswept wings through the transonic speed range
have been made by the modified strip-theory method of NACA RM L57L10, which employs …

FLUTTER studies were begun at MIT in 1926. v. Baumhauer and Koning's fundamental
work1 on flexural-aileron flutter had just been followed by that of Blenk and Liebers'2 on …

This note attempts to clarify some basic ideas, and correct some common
misunderstandings, on wing flexure-torsion flutter. Topics include:(i) an understanding of the …

This paper is concerned with a discussion of some of the problems of flutter and
aeroelasticity that are or may be important at high speeds. Various theoretical procedures for …

Explicit solutions are obtained for the bending-torsion flutter of a two-dimensional airfoil in
incompressible flow under the assumptions that the Theodorsen function, C (k) is set equal …

Subsonic and supersonic flutter calculations have been made by the method of NACA
Research Memorandum L57L10 for 12 swept and unswept wings in order to evaluate the …