D. S. Woolston

发表

Some effects of system nonlinearities in the problem of aircraft flutter

T. A. Byrdsong, Harry L. Runyan, Donald S. Woolston, 1955 .

An Investigation of Effects of Certain Types of Structural NonHnearities on Wing and Control Surface Flutter

Robert E. Andrews, Harry L. Runyan, Donald S. Woolston, 1957 .

Response of orbit determination systems to model errors

H. Wolf, D. S. Woolston, R. K. Squires, 1969 .

Some effects of variations in several parameters including fluid density on the flutter speed of light uniform cantilever wings

D. S. Woolston, George E. Castile, 1951 .

A theoretical and experimental study of wind-tunnel-wall effects on oscillating air forces for two-dimensional subsonic compressible flow

A. Rainey, H. Runyan, D. S. Woolston, 1953 .

A Systematic Kernel Function Procedure for Determining Aerodynamic Forces on Oscillating or Steady Finite Wings at Subsonic Speeds

H. J. Cunningham, Herbert J. Cunningham, Donald S. Woolston, 1959 .

On the Kernel Function of the Integral Equation Relating the Lift and Downwash Distributions of Oscillating Finite Wings in Subsonic Flow

Harry L. Runyan, Donald S. Woolston, Charles E. Watkins, 1955 .

Method for calculating the aerodynamic loading on an oscillating finite wing in subsonic and sonic flow

Harry L. Runyan, Donald S. Woolston, H. Runyan, 1956 .

Theoretical and experimental investigation of the effect of tunnel walls on the forces on an oscillating airfoil in two-dimensional subsonic compressible flow

Harry L. Runyan, Donald S. Woolston, A. Rainey, 1956 .

Some Considerations on the Air Forces on a Wing Oscillating Between Two Walls for Subsonic Compressible Flow

D. S. Woolston, 1955 .