William J. Monta

Test description and preliminary pitot-pressure surveys for Langley Test Technique Demonstrator at Mach 6

W. J. Monta, Joel L. Everhart, George C. Ashby, 1992 .

Analysis of generic scramjet external nozzle flowfields employing simulant gases

Robert W. Walters, Kenneth E. Tatum, William J. Monta, 1990 .

New test techniques to evaluate near field effects for supersonic store carriage and separation

A. B. Blair, Robert L. Stallings, Floyd J. Wilcox, 1989 .

A parametric experimental investigation of a scramjet nozzle at Mach 6 with Freon and argon or air used for exhaust simulation

W. J. Monta, William J. Monta, J. M. Cubbage, 1991 .

PRESSURE DISTRIBUTIONS AND WAVE DRAG DUE TO TWO-DIMENSIONAL FABRICATION-TYPE SURFACE ROUGHNESS ON AN OGIVE CYLINDER AT MACH NUMBERS OF 1.61 AND 2.01

William J. Monta, K. R. Czarnecki, 1961 .

Pitot survey of exhaust flow field of a 2-D scramjet nozzle at Mach 6 with air or freon and argon used for exhaust simulation

William J. Monta, 1992 .