Lawrence E. Putnam

• Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration
• Internal pressure distributions for a two-dimensional thrust-reversing nozzle operating at a free-stream mach number of zero
• Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20