A. G. Rainey

发表

Buffeting during atmospheric ascent, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

H. A. Cole, A. L. Erickson, A. G. Rainey, 1964 .

Aeroelastic considerations for transports of the future - Subsonic, supersonic, and hypersonic.

A. G. Rainey, 1968 .

Effects of flexibility on lift and pitching- moment characteristics of a series of low- aspect-ratio wing-body combinations at transonic speeds

A. G. Rainey, R. V. Doggett, A. Rainey, 1968 .

Launch-vehicle dynamics

A. G. Rainey, Harry L. Runyan, 1961 .

Wind-tunnel flutter tests at Mach numbers up to 3.0 of Boeing wing models for weapons system 110A : COORD. No. AF-AM-108

A. G. Rainey, G. M. Levey, W. J. Tuovila, 1957 .

Experimental and Analytical Investigation of the Transonic and Supersonic Divergence Characteristics of a Delta-Plan-Form All- Movable Control

A. G. Rainey, P. W. Hanson, D. J. Martin, 1958 .

Dynamic and aeroelastic considerations of hypersonic aircraft

A. G. Rainey, D. J. Martin, 1967 .

Buffeting during atmospheric ascent - Space vehicle design criteria /structures/

H. A. Cole, A. L. Erickson, A. G. Rainey, 1970 .

On the prediction of critical flutter conditions from subcritical response data and some related wind tunnel experience

A. G. Rainey, John C. Houbolt, A. Rainey, 1958 .

Wind tunnel techniques for the study of aeroelastic effects on aircraft stability, control, and loads

A. G. Rainey, I. Abel, 1970 .

Progress on the launch-vehicle buffeting problem (Fluctuating pressure and structural response to aerodynamic input in launch vehicle buffeting)

A. G. Rainey, 1964 .

Active control of aeroelastic response

A. G. Rainey, C. L. Ruhlin, M. C. Sandford, 1972 .

Control considerations in severe turbulence

W. D. Grantham, A. G. Rainey, W. P. Gilbert, 1971 .

An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics

A. G. Rainey, R. V. Doggett, A. Rainey, 1959 .

Progress on the launch-vehicle buffeting problem

A. G. Rainey, A. Rainey, 1965 .