L. E. Putnam

The effect of throat contouring on two-dimensional converging-diverging nozzles at static conditions

M. L. Mason, L. E. Putnam, R. J. Re · NASA STI Repository (National Aeronautics and Space Administration) · 1980 · 82 citations · Full text

Aeroacoustics, Engineering, Fluid Mechanics +17

Results of AGARD assessment of prediction capabilities for nozzle afterbody flows

L. E. Putnam, Norbert Bissinger · 21st Joint Propulsion Conference · 1985 · 19 citations

Aeroacoustics, Nozzle Afterbody, Unsteady Flow +13

Experimental determination of equivalent solid bodies to represent jets exhausting into a Mach 2.20 external stream

F. J. Capone, L. E. Putnam · NASA Technical Reports Server (NASA) · 1969 · 19 citations

Engineering, Fluid Mechanics, Mechanical Engineering +6

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

L. E. Putnam, C. E. Mercer · NASA Technical Reports Server (NASA) · 14 citations · Full text

Rectangular Nozzle, Aeroacoustics, Unsteady Flow +14

Investigation of effects of ramp span and deflection angle on laminar boundary-layer separation at mach 10.03

L. E. Putnam · NASA Technical Reports Server (NASA) · 1965 · 10 citations · Full text

Engineering, Laminar Boundary-layer Separation, Aerospace Engineering +10