H. Runyan

发表

Effect of high-velocity fluid flow on the bending vibrations and static divergence of a simply supported pipe

H. L. Dodds, Harry L. Runyan, H. Dodds, 1965 .

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 .

Procedure for calculating flutter at high supersonic speed including camber deflections, and comparison with experimental results

H. Runyan, H. G. Morgan, V. Huckel, 1958 .

Theoretical Considerations of Flutter at High Mach Numbers

Harry L. Runyan, H. Runyan, H. G. Morgan, 1958 .

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 .

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 .

Experimental Investigation of the Effects of Concentrated Weights on Flutter Characteristics of a Straight Cantilever Wing

J. L. Sewall, Harry L Runyan, John L Sewall, 1948 .

Unsteady lifting surface theory applied to a propeller and helicopter rotor

Harry L. Runyan, H. Runyan, 1973 .

Theoretical Investigation of Several Types of Single Degree of Freedom Flutter

H. Runyan, 1952 .

Effect of a flexibly mounted store on the flutter speed of a wing

H. L. Runyan, H. Runyan, 1980 .

Flutter of a uniform wing with an arbitrarily placed mass according to a differential-equation analysis and a comparison with experiment

Harry L. Runyan, Charles E. Watkins, C. E. Watkins, 1949 .

A review of rotating blade noise technology

H. L. Runyan, H. H. Hubbard, D. L. Lansing, 1971 .

SINGLE-DEGREE-OF-FREEDOM-FLUTTER CALCULATIONS FOR A’ WING IN SUBSONIC POTENTIAL FLOW AND COMPARISON WITH AN l$XPERItiENT

H. Runyan, Harry L Runyan, HAltRY L. Runyan, 2000 .

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 .

Sonic‐Boom Propagation through a Stratified Atmosphere

Harry L. Runyan, W. Hayes, H. Runyan, 1972 .

Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow

Harry L. Runyan, Charles E. Watkins, C. E. Watkins, 1951 .

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 Recent Information on Aircraft Vibration Due to Aerodynamic Sources

Harry L. Runyan, H. Runyan, 1968 .

Decoupler Pylon: A Simple, Effective Wing/Store Flutter Suppressor

J. T. Foughner, W. H. Reed, Harry L. Runyan, 1980 .