Investigation of the Effects of a Nacelle on the Aerodynamic Characteristics of a Swept Wing and the Effects of Sweep on a Wing Alone
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WIND TUNNEL TESTS - NACA - HIGH-SPEED (16')↗
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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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Investigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wings
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AIRFOILS - NACA 0012↗
Theoretical lift and damping in roll of thin sweptback wings of arbitrary taper and sweep at supersonic speeds subsonic leading edges and supersonic trailing edges
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DAMPING IN ROLL↗
Theoretical Basic Span Loading Characteristics of Wings with Arbitrary Sweep, Aspect Ratio, and Taper Ratio
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Stevens, Victor I↗
Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds : supersonic leading and trailing edges
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WINGS, THIN - STABILITY↗
Theoretical supersonic characteristics of inboard trailing-edge flaps having arbitrary sweep and taper : Mach lines behind flap leading and trailing edges
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CONTROL SURFACES - EFFECT OF SWEEPBACK↗
Study of Effects of Sweep on the Flutter of Cantilever Wings
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Barmby, J G↗
Lift, pitching moment, and span load characteristics of wings at low speed as affected by variations of sweep and aspect ratio
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LOAD DISTRIBUTION, WING-SPAN↗
Effects of wing sweep on the upwash at the propeller planes of multiengine airplanes
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Rogallo, Vernon L↗
Theoretical investigation of the supersonic lift and drag of thin, sweptback wings with increased sweep near the root
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Cohen, Doris↗
Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds
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Turner, Thomas R↗
Effects of Sweep and Angle of Attack on Boundary-layer Transition on Wings at Mach Number 4.04
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Dunning, Robert W↗
Effect of sweep on performance of compressor blade sections as indicated by swept-blade rotor, unswept-blade rotor, and cascade tests
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Godwin, William R↗
Investigation of Deflectors as Gust Alleviators on a 0.09-scale Model of the Bell X-5 Airplane with Various Wing Sweep Angles from 20 Degrees to 60 Degrees at Mach Numbers from 0.40 to 0.90
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Croom, Delwin R↗
Wind-tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack up to 13 Degrees and at High Subsonic Mach Numbers, Including a Semiempirical Method of Estimating the Rolling Derivatives
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Wiggins, James W↗
Low-speed Experimental Determination of the Effects of Leading-edge Radius and Profile Thickness on Static and Oscillatory Lateral Stability Derivatives for a Delta Wing with 60 Degrees of Leading-edge Sweep
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Fletcher, Herman S↗
An investigation of the downwash behind a high-aspect-ratio wing with various amounts of sweep in the Langley 8-foot high-speed tunnel
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Whitcomb, Richard T↗
Effects of sweep on controls
An analysis of the principal results of recent control-surface research pertinent to transonic flight has been made. An indication of the nature of the changes in control-surface characteristics above the critical speed of the wing and a preliminary design procedure for estimating the effectiveness of flap-type controls on swept wings are presented.
CONTROLS, FLAP TYPE - COMPLETE WINGS↗