Irwin E. Vas

发表

Lunar and planetary landers for human exploration missions

Gordon Woodcock, Michael L. Cupples, Jill A. Nordwall, 1992 .

DOWNSTREAM EFFECTS OF BLUNTNESS IN THE MERGED FLOW REGIME**This work was supported by the Air Force Office of Scientific Research under its contract F44620-71-C-0032 and by the National Science Foundation, NSF Grant GK-31204X.

Irwin E. Vas, James G. Sierchio, 1974 .

Wind Energy Innovative Systems conference proceedings

Irwin E. Vas, 1979 .

Validation of CFD for aircraft design: A Boeing view

Hideo Yoshihara, Paul E. Rubbert, Irwin E. Vas, 1987 .

Reynolds Number Effects on Shock-Wave Turbulent Boundary-Layer Interactions

Gary S. Settles, Irwin E. Vas, C. C. Horstman, 1977 .

Details of a Shock-Separated Turbulent Boundary Layer at a Compression Corner

Gary S. Settles, Irwin E. Vas, Seymour M. Bogdonoff, 1976 .

Incipient Separation of a Supersonic Turbulent Boundary Layer at High Reynolds Numbers

Gary S. Settles, Irwin E. Vas, Seymour M. Bogdonoff, 1976 .

Preliminary Investigations of Spiked Bodies at Hypersonic Speeds

Irwin E. Vas, Seymour M. Bogdonoff, I. Vas, 1959 .

Shock wave-turbulent boundary layer interaction at a high Reynolds number, including separation and flowfield measurements

Gary S. Settles, Irwin E. Vas, Seymour M. Bogdonoff, 1976 .

Space Station Reboost with Electrodynamic Tethers

Ethan A. Scarl, Irwin E. Vas, T. Kelly, 2000 .