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Forrest E Gowen

Observed names: F. GOWEN, FORREST E. GOWEN, Forrest E. Gowen, Forrest R Gowen, Gowen, F. E., Gowen, Forrest E, Gowen, Forrest E.
OpenAlex ID: A5015502452
Drag of Circular Cylinders for a Wide Range of Reynolds Numbers and Mach Numbers
1953 · Forrest E Gowen, Edward W Perkins · NASA STI Repository (National Aeronautics and Space Administration) · 62
Gain and power of CO2 gasdynamic lasers.
1972 · GEORGE LEE, FORREST E. GOWEN, et al. · AIAA Journal · 34
Gain of Co2 Gasdynamic Lasers
1971 · George Lee, Forrest E. Gowen · Applied Physics Letters · 30
A Study of the Effects of Body Shape on the Vortex Wakes of Inclined Bodies at a Mach Number of 2
1953 · Forrest E Gowen, Edward W Perkins · 22
Design and performance of a combined radiative- convective heating facility
1971 · F. GOWEN, D. PETERSON, et al. · AIAA Aerodynamic Measurement Technology and Ground Testing Conference · 8
Buffeting of a Vertical Tail on an Inclined Body at Supersonic Mach Numbers
1953 · Forrest E Gowen · NASA STI Repository (National Aeronautics and Space Administration) · 6
The Ames combined heating facility
1969 · F. GOWEN, F. NICHOLS · AIAA Aerodynamic Measurement Technology and Ground Testing Conference · 2
A Wind Tunnel Using Arc-heated Air for Mach Numbers From 10 to 20
1962 · Forrest E Gowen, V. D. Hopkins · NASA Technical Reports Server (NASA) · 2
Heat-transfer and Boundary-layer Transition on a Heated 20 Degree Cone at a Mach Number of 1.53
1949 · Richard Scherrer, Forrest R Gowen, et al. · NASA STI Repository (National Aeronautics and Space Administration) · 2
The change with mass-flow ratio of the cowl pressure drag of normal-shock inlets at supersonic speeds
1956 · Wallace F Davis, Forrest E Gowen · NASA STI Repository (National Aeronautics and Space Administration) · 1
Preliminary experimental investigation of a variable-area, variable-internal-contraction air inlet at Mach numbers between 1.42 and 2.44
1955 · Richard Scherrer, Forrest E Gowen · 1
Research Memorandum Preliminary Experjmental Investigation of a Variable-area, Varlable-internalcontraction Air Inlet at Mach
1955 · Richard Schemer, Forrest E Gowen
NACA Technical Notes
1953 · Gowen, Forrest E., Perkins, Edward W. · University of North Texas Digital Library (University of North Texas)
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NACA Research Memorandums
1952 · Gowen, Forrest E., Perkins, Edward W. · University of North Texas Digital Library (University of North Texas)
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NACA Research Memorandums
1951 · Seiff, Alvin, Sandahl, Carl A., et al. · University of North Texas Digital Library (University of North Texas)
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Flow Over Inclined Bodies
1951 · Edward W Perkins, Forrest E Gowen · NASA Technical Reports Server (NASA)
Aerodynamic characteristics of the NACA RM-10 research missile in the Ames 1- by 3-foot supersonic wind tunnel no. 2 : pressure and force measurements at Mach numbers of 1.52 and 1.98
1951 · Edward W Perkins, Forrest E Gowen, et al. · NASA Technical Reports Server (NASA)
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Comparison of Theoretical and Experimental Heat Transfer on a Cooled 20 Degrees Cone with a Laminar Boundary Layer at a Mach Number of 2.02
1950 · Richard Scherrer, Forrest E Gowen
NACA Research Memorandums
1948 · Perkins, Edward W., Gowen, Forrest E., et al. · University of North Texas Digital Library (University of North Texas)
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NACA Research Memorandums
1948 · Scherrer, Richard, Wimbrow, William R., et al. · University of North Texas Digital Library (University of North Texas)
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NACA Technical Notes
1947 · Scherrer, Richard, Gowen, Forrest E. · University of North Texas Digital Library (University of North Texas)
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Works count: 27
Citation count: 170
H-index: 6
I10-index: 4
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