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Raymond E Mineck

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Flight testsApplication of two procedures for dual-point design of transonic airfoilsRaymond E. Mineck

Application of two procedures for dual-point design of transonic airfoils

Raymond E. Mineck · National Aeronautics and Space Administration, Langley Research Center

Sayfa sayısı yok · 1994

Aerodynamic coefficients / Aircraft landing / F-15 aircraft / Flight control / Flight tests

WingsWind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord lineRaymond E. Mineck

Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line

Raymond E. Mineck · National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program

Sayfa sayısı yok · 1993

Wind tunnels / Airplanes / Wings

Interference (Aerodynamics)Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniquesRaymond E. Mineck

Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques

Raymond E. Mineck · For sale by the National Technical Information Service]

69 sayfa · 1992

Wind tunnel walls / Adaptive-wall wind tunnels / Interference / Interference (Aerodynamics)

Navier-Stokes equationStudy of potential aerodynamic benefits from spanwise blowing at wingtipRaymond E. Mineck

Study of potential aerodynamic benefits from spanwise blowing at wingtip

Raymond E. Mineck · National Aeronautics and Space Administration, Langley Research Center

Sayfa sayısı yok · 1995

Aerodynamic drag / Aerodynamics / Commercial aircraft / Lift / Navier-Stokes equation

Wind tunnel wallsWall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test sectionRaymond E. Mineck

Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section

Raymond E. Mineck · National Aeronautics and Space Administration, Scientific and Technical Information Division

96 sayfa · 1987

Airfoils / Aerodynamics / Correction / Interference / Wind tunnel walls

CiltComputer model to simulate testing at the National Transonic FacilityRaymond E. Mineck

Computer model to simulate testing at the National Transonic Facility

Raymond E. Mineck · National Technical Information Service, distributor

Sayfa sayısı yok · 1995

Kategori yok

AileronsReynolds number effects on the performance of lateral control devicesRaymond E. Mineck

Reynolds number effects on the performance of lateral control devices

Raymond E. Mineck · National Technical Information Service, distributor

Sayfa sayısı yok · 2000

Reynolds number / Spoilers / Lateral control / Ailerons

TurbulenceSteady and periodic pressure measurements on a generic helicopter fuselage model in the presence of a rotorRaymond E. Mineck

Steady and periodic pressure measurements on a generic helicopter fuselage model in the presence of a rotor

Raymond E. Mineck · National Aeronautics and Space Administration, Langley Research Center

183 sayfa · 2000

Measurement / Rotors (Helicopters) / Pressure / Testing / Turbulence

Aerodynamic characteristicsEffect of full-chord porosity on aerodynamic characteristics of the NACA 0012 airfoilRaymond E. Mineck

Effect of full-chord porosity on aerodynamic characteristics of the NACA 0012 airfoil

Raymond E. Mineck · Langley Research Center

88 sayfa · 1996

Airfoils / Aerodynamic characteristics

CalibrationCalibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic TunnelRaymond E. Mineck

Calibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic Tunnel

Raymond E. Mineck · National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division

Sayfa sayısı yok · 1990

Transonic wind tunnels / Wind tunnel walls / Calibration

WingsWind-tunnel investigation of aerodynamic efficiency of three planar elliptical wings with curvature of quarter-chord lineRaymond E. Mineck

Wind-tunnel investigation of aerodynamic efficiency of three planar elliptical wings with curvature of quarter-chord line

Raymond E. Mineck · Langley Research Center

78 sayfa · 1993

Wind tunnel tests / Wings

AirplanesAssessment of potential aerodynamic benefits from spanwise blowing at the wingtipRaymond E. Mineck

Assessment of potential aerodynamic benefits from spanwise blowing at the wingtip

Raymond E. Mineck · For sale by the National Technical Information Service

Sayfa sayısı yok · 1992

Wings, Swept-back / Airplanes

Stability of helicoptersEffect of rotor wake on aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraftRaymond E Mineck

Effect of rotor wake on aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft

Raymond E Mineck · National Aeronautics and Space Administration

118 sayfa · 1977

Aerodynamics / Rotors (Helicopters) / Stability of helicopters

AerofoilsHigh Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnelRaymond E. Mineck

High Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel

Raymond E. Mineck · For sale by the National Technical Information Service]

Sayfa sayısı yok · 1987

Reynolds number / Transonic wind tunnels / Testing / Aerofoils

ResearchHardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic tunnelRaymond E. Mineck

Hardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic tunnel

Raymond E. Mineck · For sale by the National Technical Information Service

Sayfa sayısı yok · 1989

Aeronautics / Research

Wind tunnelsApplication of an unstructured grid Navier-Stokes solver to a generic helicopter bodyRaymond E. Mineck

Application of an unstructured grid Navier-Stokes solver to a generic helicopter body

Raymond E. Mineck · Available from NASA Center for AeroSpace Information

47 sayfa · 1999

Measurement / Rotors (Helicopters) / Testing / Aerodynamics / Wind tunnels