M. L. Mason

Experimental Study of an Axisymmetric Dual Throat Fluidic Thrust Vectoring Nozzle for Supersonic Aircraft Application

Jeffrey D. Flamm, Karen Deere, M. L. Mason et al. · 2007 · 88 citations · Full text

Dual Throat Nozzle, Aeroacoustics, Unsteady Flow +14

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

Design Enhancements of the Two-Dimensional, Dual Throat Fluidic Thrust Vectoring Nozzle Concept

Jeffrey D. Flamm, Karen Deere, M. L. Mason et al. · 3rd AIAA Flow Control Conference · 2006 · 72 citations · Full text

Aeroacoustics, Unsteady Flow, Engineering +14

Experimental Study of a Dual-Throat Fluidic Thrust-Vectoring Nozzle Concept

Jeffrey D. Flamm, Karen Deere, B. L. Berrier et al. · 2005 · 35 citations

Unsteady Flow, Engineering, Aerospace Engineering +7

Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring

B. L. Berrier, M. L. Mason · NASA Technical Reports Server (NASA) · 1988 · 24 citations

Unsteady Flow, Engineering, Axisymmetric Nozzle +14