Search results for: Mineck, Raymond E.
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1
Hardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic tunnel
Authors: Mineck, Raymond E.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1989Physical Description: 1 volume.Holdings: Loading…
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2
Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section
Authors: Mineck, Raymond E.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987Physical Description: 1 volume.Holdings: Loading…
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3
High Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
Authors: Mineck, Raymond E.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1987Physical Description: 1 volume.Holdings: Loading…
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4
Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques
Authors: Mineck, Raymond 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
Calibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic Tunnel
Authors: Mineck, Raymond E.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1990Physical Description: 1 volume.Holdings: Loading…
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6
Assessment of potential aerodynamic benefits from spanwise blowing at the wingtip
Authors: Mineck, Raymond E.
Published: National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1992Physical Description: 1 volume.Holdings: Loading…
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7
Effect of rotor wake on aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft
Authors: Mineck, Raymond E.
Physical Description: 118 pages : illustrations ; 27 cm.Holdings: Loading…
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8
Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line
Authors: Mineck, Raymond 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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9
Application of two procedures for dual-point design of transonic airfoils
Authors: Mineck, Raymond 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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10
Reynolds number effects on the performance of lateral control devices
Authors: Mineck, Raymond E.
Published: National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 2000Physical Description: 1 volume.Holdings: Loading…
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11
Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section
Authors: Mineck, Raymond E.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987Physical Description: 1 online resource (96 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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12
Reynolds number effects on the performance of lateral control devices
Authors: Mineck, Raymond E.
Published: National Aeronautics and Space Administration, Langley Research Center, 2000Physical Description: 1 online resource (139 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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13
Wind-tunnel test of an articulated helicopter rotor model with several tip shapes
Authors: Berry, John D.Other Authors: “…Mineck, Raymond E.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1980
Physical Description: 92 pages : chiefly illustrations ; 27 cm.Holdings: Loading…
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14
Adaptive wind tunnel walls : a selected, annotated bibliograpy
Authors: Tuttle, Marie H.Other Authors: “…Mineck, Raymond E.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1986
Physical Description: 1 volume.Holdings: Loading…
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15
An improved computational procedure for determining helicopter rotor blade natural modes
Authors: Weller, William H.Other Authors: “…Mineck, Raymond E.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978
Physical Description: 85 pages : illustrations ; 27 cm.Holdings: Loading…
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16
Computer model to simulate testing at the National Transonic Facility
Published: National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995Other Authors: “…Mineck, Raymond E.…”
Physical Description: 1 volume.Holdings: Loading…
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17
Aerodynamic characteristics and pressure distributions for an executive-jet baseline airfoil section
Authors: Allison, Dennis O.Other Authors: “…Mineck, Raymond E.…”
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1993
Physical Description: 1 volume.Holdings: Loading…
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18
Assessment of dual-point drag reduction for an executive-jet modified airfoil section
Authors: Allison, Dennis O.Other Authors: “…Mineck, Raymond E.…”
Published: National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1996
Physical Description: 1 volume.Holdings: Loading…
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19
Wind tunnel wall interference in V/STOL and high lift testing : a selected, annotated bibliography
Authors: Tuttle, Marie H.Other Authors: “…Mineck, Raymond E.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986
Physical Description: 1 volume.Holdings: Loading…
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Related Subjects
Aerodynamics
Reynolds number
Transonic wind tunnels
Wind tunnel walls
Aerofoils
Rotors (Helicopters)
Testing
Wind tunnels
Ailerons
Airfoil profiles
Airplanes
Cryogenic wind tunnels
Lateral control
Spoilers
Wind tunnel tests
Aerodynamic characteristics
Aerodynamic coefficients
Aeronautics
Aircraft landing
Angle of attack
Boundary layer transition
COMPUTERIZED SIMULATION
Calibration
Drag reduction
F-15 aircraft
Flight control
Flight tests
Force distribution
Ground effect (Aerodynamics)
Ground simulators