Ivan E. Beckwith

发表

Development of square nozzles for supersonic low-disturbance wind tunnels

Steven P. Schneider, John J. Korte, Jeffery A. White, 1996 .

The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section

Ivan E. Beckwith, Herbert W. Ridyard, Nancy Cromer, 1952 .

Design and fabrication requirements for low-noise supersonic/hypersonic wind tunnels

I. E. Beckwith, Ivan E. Beckwith, Mujeeb R. Malik, 1988 .

On the design of a new Mach 3.5 quiet nozzle

Ivan E. Beckwith, Fang-Jenq Chen, Mujeeb R. Malik, 1990 .

Gortler instability and supersonic quiet nozzle design

Ivan E. Beckwith, Mujeeb R. Malik, Fang-Jeng Chen, 1992 .

Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number

I. E. Beckwith, Ivan E. Beckwith, Eli Reshotko, 1957 .

Heat Transfer and Recovery Temperatures on a Sphere with Laminar, Transitional, and Turbulent Boundary Layers at Mach Numbers of 2.00 and 4.15

I. E. Beckwith, Ivan E. Beckwith, James J. Gallagher, 1957 .

Experimental and theoretical investigation of boundary-layer instability mechanisms on a swept leading edge at Mach 3.5

I. E. Beckwith, Ivan E. Beckwith, Mujeeb R. Malik, 1987 .

Gortler vortices and transition in wall boundary layers of two Mach 5 nozzles

I. E. Beckwith, Ivan E. Beckwith, Barbara B. Holley, 1981 .

Local Heat Transfer and Recovery Temperatures on a Yawed Cylinder at a Mach Number of 4.15 and High Reynolds Numbers

I. E. Beckwith, Ivan E. Beckwith, James J. Gallagher, 1961 .

Development of a high Reynolds number quiet tunnel for transition research

I. E. Beckwith, Ivan E. Beckwith, 1974 .

Goertler instability and hypersonic quiet nozzle design

I. E. Beckwith, Ivan E. Beckwith, Fang-Jenq Chen, 1991 .