D. Boldman

发表

Laminarization of a turbulent boundary layer as observed from heat-transfer and boundary layer measurements in conical nozzles

A. K. Gallagher, J. Schmidt, D. Boldman, 1968 .

NOZZLES WITH VARIOUS DIAMETER UNCOOLED PIPE INLETS HALF-ANGLE OF CONVERGENCE

James F. Schmidt, D. Boldman, Harvey E. Nenmann, 1967 .

Turbulence, Heat-Transfer, and Boundary Layer Measurements in a Conical Nozzle with a Controlled Inlet Velocity Profile.

James F. Schmidt, A. Fortini, D. Boldman, 1966 .

Similar solutions for turbulent boundary layer with large favorable pressure gradients /nozzle flow with heat transfer/

J. Schmidt, D. Boldman, C. Todd, 1971 .

Three-dimensional fluid flow phenomena in the blade end wall corner region

R. Raj, D. Boldman, B. Hazarika, 1986 .

Velocity, intermittency, and turbulence intensity measurements in the boundary layer of an accelerated flow

H. E. Neumann, R. C. Ehlers, D. Boldman, 1970 .

Experimental and analytical study of a conically diffused flow with a nearly separated boundary layer

H. E. Neumann, D. Boldman, 1973 .

Heat transfer and boundary layer in conical nozzles

R. Graham, D. Boldman, R. Summa, 1972 .

N O T I C E THIS DOCUMENT HAS BEEN REPRODUCED FROM MICROFICHE. ALTHOUGH IT IS RECOGNIZED THAT CERTAIN PORTIONS ARE ILLEGIBLE, IT IS BEING RELEASED IN THE INTEREST OF MAKING AVAILABLE AS MUCH INFORMATION AS POSSIBLE

D. Boldman, A. Buggele, Michelson, 2009 .

Vortex shedding from a blunt trailing edge with equal and unequal external mean velocities

M. E. Goldstein, D. R. Boldman, P. F. Brinich, 1975, Journal of Fluid Mechanics.

The 3-D viscous flow CFD analysis of the propeller effect on an advanced ducted propeller subsonic inlet

M. Ibrahim, D. Boldman, C. Iek, 1993 .

Analysis of an advanced ducted propeller subsonic inlet

Mounir B. Ibrahim, Donald R. Boldman, Chanthy Iek, 1995 .

Wall Shear Stress Measurement in Blade End-Wall Corner Region

R. Raj, R. Bhargava, D. Boldman, 1987 .

Effect of a rotating propeller on the separation angle of attack and distortion in ducted propeller inlets

D. R. Boldman, C. Iek, D. P. Hwang, 1993 .

Evaluation of panel code predictions with experimental results of inlet performance for a 17-inch ducted prop/fan simulator operating at Mach 0.2

R. J. Jeracki, D. R. Boldman, C. Iek, 1991 .

Mean Velocity, Turbulence Intensity, and Scale in a Subsonic Turbulent Jet Impinging Normal to a Large Flat Plate

P. F. Brinich, D. Boldman, 1977 .

Flow analysis for the nacelle of an advanced ducted propeller at high angle-of-attack and at cruise with boundary layer control

D. Boldman, C. Hughes, D. Hwang, 1994 .

Skin friction on a flat perforated acoustic liner

D. R. Boldman, P. F. Brinich, D. Boldman, 1976 .