Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles / Ivan E. Beckwith and Barbara B. Holley.Ivan E. Beckwith1981
Fluctuating properties of turbulent boundary layers for Mach numbers up to 9 / William D. Harvey, Dennis M. Bushnell, and Ivan E. Beckwith.William Harvey1969
Noise reduction in a Mach 5 wind tunnel with a rectangular rod-wall sound shield / Theodore R. Creel, Jr., J. Wayne Keyes, and Ivan E. Beckwith.Theodore R. Creel1980
Local Heat Transfer and Recovery Temperatures on a Yawed Cylinder at a Mach Number of 4.15 and High Reynolds Numbers, by Ivan E. Beckwith and James J. Gallagher.Ivan E. Beckwith1961
Comparisons of Turbulent-boundary-layer Measurements at Mach Number 19.5 with Theory and an Assessment of Probe Errors by Ivan E. Beckwith, William D. Harvey, and Frank L. Clark.Ivan E. Beckwith1971
Effects of a Modified Leading Edge on Noise and Boundary-layer Transition in a Rod-wall Sound Shield at Mach 5 / Theodore R. Creel, Jr., Barbara B. Holley, and Ivan E. Beckwith.Theodore R. Creel1981