D. R. Boldman

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 .

Experimental evaluation of shockless supercritical airfoils in cascade

D. R. Boldman, L. M. Shaw, A. E. Buggele, 1983 .

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.

Skin friction on a flat perforated acoustic liner

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

Three-dimensional shock structure in a transonic flutter cascade

D. R. Boldman, A. J. Decker, A. E. Buggele, 1982 .

Unsteady Pressure Measurements on a Biconvex Airfoil in a Transonic Oscillating Cascade

D. R. Boldman, L. M. Shaw, A. E. Buggele, 1986 .

Wind tunnel tests of a blade subjected to midchord torsional oscillation at high subsonic stall flutter conditions

D. R. Boldman, A. E. Buggele, 1978 .