P. F. Bradley

发表

Comparison of Shuttle Orbiter Surface Pressures with Wind Tunnel and Theoretical Predictions

P. M. Siemers, P. F. Bradley, K. J. Weilmuenster, 1984 .

Shuttle flight pressure instrumentation: Experience and lessons for the future

P. M. Siemers, P. F. Bradley, H. Wolf, 1983 .

An evaluation of Space Shuttle Orbiter forward fuselage surface pressures - Comparison with wind tunnel and theoretical predictions

P. M. Siemers, P. F. Bradley, K. J. Weilmuenster, 1983 .

Pressure distributions obtained on a 0.04-scale and 0.02-scale model of the Space Shuttle Orbiter's forward fuselage in the Langley 20-inch Mach 6 air tunnel

P. M. Siemers, P. F. Bradley, P. F. Flanagan, 1983 .

Pressure distributions on a 0.04-scale model of the Space Shuttle Orbiter's forward fuselage in the Langley unitary plan wind tunnel

P. M. Siemers, P. F. Bradley, P. F. Flanagan, 1983 .

Pressure distributions obtained on a 0.04-scale and 0.02-scale model of the Space Shuttle Orbiter's forward fuselage in the Langley continuous flow hypersonic tunnel

P. M. Siemers, P. F. Bradley, P. F. Flanagan, 1983 .

Space Shuttle Orbiter flight heating rate measurement sensitivity to thermal protection system uncertainties

P. F. Bradley, D. A. Throckmorton, 1981 .

Vectorized schemes for conical potential flow using the artificial density method

P. F. Bradley, Jerry C. South, Douglas L. Dwoyer, 1984 .