Search results for: Erickson, Gary E.
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1
On the nonlinear aerodynamic and stability characteristics of a generic chine-forebody slender-wing fighter configuration
Authors: Erickson, Gary E.
Published: National Aeronautics and Space Administration, Ames Research Center ; [For sale by the National Technical Information Service], 1987Physical Description: 1 volume.Holdings: Loading…
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2
Wind tunnel investigation of vortex flows on F/A-18 configuration at subsonic through transonic speeds
Authors: Erickson, Gary E.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1991Physical Description: 1 volume.Holdings: Loading…
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3
Wind tunnel investigation of the interaction and breakdown characteristics of slender-wing vortices at subsonic, transonic, and supersonic speeds
Authors: Erickson, Gary E.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1991Physical Description: 1 volume.Holdings: Loading…
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4
Effects of forebody strakes and Mach number on overall aerodynamic characteristics on configuration with 55.
Authors: Erickson, Gary E.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992Physical Description: 1 volume.Holdings: Loading…
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5
Improvement of maneuver aerodynamics by spanwise blowing
Authors: Erickson, Gary E.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1977Physical Description: 65 pages : illustrations ; 27 cm.Holdings: Loading…
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6
Wind tunnel investigations of forebody strakes for yaw control on F/A-18 model at subsonic and transonic speeds
Authors: Erickson, Gary E.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1993Physical Description: 1 volume.Holdings: Loading…
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7
Fiber-optic-based laser vapor screen flow visualization sysytem for aerodynamic research in larger scale subsonic and transonic wind tunnels
Authors: Erickson, Gary E.
Published: National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1994Physical Description: 1 volume.Holdings: Loading…
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8
Unified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields
Authors: Erickson, Gary E.
Published: National Aeronautics and Space Administration, Langley Research Center, 2010Physical Description: 1 online resource (v, 32 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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9
Estimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods
Authors: Erickson, Gary E.
Published: National Aeronautics and Space Administration, Langley Research Center, 2010Physical Description: 1 online resource (v, 36 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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10
Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique
Authors: Erickson, Gary E.
Published: National Aeronautics and Space Administration, Langley Research Center, 2013Physical Description: 1 online resource (50 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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11
Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds
Authors: Erickson, Gary E.
Published: National Aeronautics and Space Administration, Langley Research Center, 2013Physical Description: 1 online resource (521 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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12
Analysis of a split-plot experimental design applied to a low-speed wind tunnel investigation
Authors: Erickson, Gary E.
Published: National Aeronautics and Space Administration, Langley Research Center, 2013Physical Description: 1 online resource (v, 31 pages) : color illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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13
Wind tunnel investigation of passive porosity applied to the leading-edge extension and leading-edge flaps on a slender wing at subsonic speed
Authors: Erickson, Gary E.
Published: National Aeronautics and Space Administration, Langley Research Center, 2017Physical Description: 1 online resource (iv, 43 pages) : color illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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14
Wind tunnel investigation of the supersonic stage separation aerodynamics of a generic 0.0175- scale bimese two-stage-to-orbit reusable launch vehicle configuration
Authors: Erickson, Gary E.
Published: National Aeronautics and Space Administration, Langley Research Center, 2020Physical Description: 1 online resoure (iv, 545 pages, 1 unnumbered page) : illustrations (chiefly color).Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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15
Water facilities in retrospect and prospect--an illuminating tool for vehicle design
Published: National Aeronautics and Space Administration, Ames Research Center ; [For sale by the National Technical Information Service], 1986Other Authors: “…Erickson, Gary E.…”
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Related Subjects
Aerodynamics
Angle of attack
Flow visualization
Static pressure
Wind tunnels
Aerodynamic configurations
Airplanes
Leading edges
Mach number
Reynolds number
Shock waves
Subsonic speed
Vortex-motion
Vortices
Wings, Triangular
Aerodynamic characteristics
Aerodynamic coefficients
Aerodynamic drag
Aerodynamic loads
Aerodynamics, Supersonic
Aircraft models
Boundary layer separation
Canard configurations
Control surfaces
Degrees of freedom
Delta wings
Dynamic pressure
Fiber optics
Fluid mechanics
Hornet (Jet fighter plane)