Measurement of Flying Qualities of a Douglas A-26B Airplane (AAF No. 41-39120) III : Stalling Characteristics
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AIRPLANES - DOUGLAS A-26B FLIGHT TESTS (AMER )↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Flight Measurements of the Flying Qualities of an F6F-3 Airplane (Buaer No. 04776) III : Stalling Characteristics
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AIRPLANES - GRUMMAND F6F-3 FLIGHT TESTS (AMER )↗
Measurements in Flight of the Stability, Lateral Control, and Stalling Characteristics of an Airplane Equipped with Full-span Zap Flaps and Spoiler-Type Ailerons
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STABILITY & CONTROL - VOUGHT-SIKORSKY OS2U-2↗
Summary of Measurements in Langley Full-Scale Tunnel of Maximum Lift Coefficients and Stalling Characteristics of Airplanes
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STALLING CHARACTERISTICS↗
Tests of a 1/14-Scale Powered Model of the XB-36 Airplane in the Langley 19-Foot Pressure Tunnel I : Stalling Characteristics and Aileron Effectiveness of Several Wing and Flap Arrangements
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WINGS - CONSOLIDATED VULTEE B-36 WIND TUNNEL TESTS↗
Additional design charts relating to the stalling of tapered wings
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AIRFOILS - NACA 230 - CHAR↗
Effect of Mach and Reynolds Numbers on the Maximum Lift Coefficient Obtainable in Gradual and Abrupt Stalls of a Pursuit Airplane Equipped with a Low-Drag Wing
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LIFT COEFFICIENTS - BELL P-63A-6↗
Flight Measurements of Horizontal Tail Loads on a Typical Propeller-Driven Pursuit Airplane During Stalled Pull-Outs at High Speed
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MACH NUMBER↗
Flight investigation of a stall-warning indicator for operation under icing conditions
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INSTRUMENTS-PITOT TUBES↗
Analysis of Low-Speed Stall Aerodynamics of a Swept Wing with Seamless Flaps
No abstract available
CFD↗
Compute Overlap Stall (COS): Predicting Performance of Power Management for Shared Memory Codes When Throttling Processors, Memory, and Thread Concurrency
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Computer science↗
Large-scale wind-tunnel tests of an airplane model with an unswept tilt wing of aspect ratio of 5.5, and with various stall control devices
Wind-tunnel stability tests of tilt-wing vtol aircraft
WIND TUNNEL STABILITY TEST↗
Deep-stall aerodynamic characteristics of t-tail aircraft
Wind tunnel test program for study of aerodynamic characteristics of T-tail aircraft at high angles of attack
AERODYNAMIC CHARACTERISTICS↗
Tabulated pressure coefficients and aerodynamic characteristics measured in flight on the wing of the douglas d-558-i airplane for a 1 g stall, a speed run to a mach number of 0.90, and a wind-up turn at a mach number of 0.86
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Keener, E. R.↗
Effect of stall-control devices on the low- speed characteristics of swept wings. part i- fixed sweep
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Furlong, G. C.↗
Effect of stall-control devices on the low- speed characteristics of swept wings. part ii- variable sweep
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Kemp, W. B., Jr.↗
Shock stalled flows for supersonic type airfoils at transonic speeds
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Stack, J.↗
Experimental investigation of dynamic distortion in a Mach 2.50 inlet with 60 percent internal contraction and its effect on turbojet stall margin
Dynamic distortion of supersonic wind tunnel for turbojet engines
Calogeras, J. E.↗