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Determination of indicial lift and moment of a two-dimensional ptiching airfoil at subsonic Mach numbers from oscillatory coefficients with numerical calculations for a Mach number... by Mazelsky, Bernard

Calculations of derivatives for rectangular wings of finite span by Cicala's method / by Jones, William Neville Prichard

Natural frequencies of vibration for a wing carrying engines / by Dalton, G. C. J.

Note on the calculation of vibration frequencies for an aero-engine installation / by Dalton, G. C. J.

Application of response function to calculation of flutter characteristics of a wing carrying concentrated masses / by Serbin, H.

Effect of various parameters including Mach number on the single-degree-of-freedom flutter of a control surface in potential flow / by Runyan, Harry L.

Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow / by Runyan, Harry L.

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Numerical determination of indicial lift of a two-dimensional sinking airfoil at subsonic Mach numbers from oscillatory lift coefficients with calculations for Mach number 0.7 / by Mazelsky, Bernard

Development and analysis of a passive vibration isolation stage for a space station precision deployable structures laboratory / by Domber, Jeanette Leah

Vibratory stresses in propellers operating in the flow field of a wing-nacelle-fuselage combination / by Rogallo, Vernon L.

Aries rocket flight vibration environment, TEM-2, multispectral measurements program / by Steeves, Russell G.

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Some effects of aspect ratio and tail length on the contribution of a vertical tail to unsteady lateral damping and directional stability of a model oscillating continuously in yaw... by Fisher, Lewis R.

A preliminary study of the problem of designing high-speed airplanes with satisfactory inherent damping of the Dutch roll oscillation / by Campbell, John P.

A flight investigation of the effect of steady rolling on the natural frequencies of a body-tail combination / by Bergrun, Norman R.

An exploratory investigation of some types of aeroelastic instability of open and closed bodies of revolution mounted on slender struts / by Clevenson, S. A.

Comparison of flutter calculations using various aerodynamic coefficients with experimental results for some rectangular cantilever wings at Mach number 1.3 / by Nelson, Herbert C.

Description and analysis of a rocket-vehicle experiment on flutter involving wing deformation and body motions / by Cunningham, Herbert J.

Some considerations on two-dimensional thin airfoils deforming in supersonic flow / by Migotsky, Eugene

Some effects of system nonlinearities in the problem of aircraft flutter / by Woolston, Donald S.

Some effects of fuselage flexibility on longitudinal stability and control / by Klawans, Bernard B.