Wind-tunnel investigation of control-surface characteristics XIII : various flap overhangs used with a 30-percent-chord flap in an NACA 66-009 airfoil
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WING FLAPS, BALANCED↗
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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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Wind-tunnel investigation of a plain and a slot-lip aileron on a wing with a full-span flap consisting of an inboard fowler and an outboard slotted flap
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WING FLAPS, FOWLER & SLOTTED & AILERONS, SEALED-GA↗
Aerodynamic Characteristics and Flap Loads of the Brake-Flap Installation on the 0.40-Scale Model of the F4F-3 Left Wing Panel
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WING PANELS - GRUMMAN F4F-3↗
Wind-tunnel investigation of plain ailerons for a wing with a full-span flap consisting of an inboard Fowler and an outboard retractable split flap
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WING FLAPS, DUPLEX↗
Aerodynamic Characteristics and Flap Loads of Perforated Double Split Flaps on a Rectangular NACA 23012 Airfoil
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WING FLAPS, SPLIT (DOUBLE)(PERFORATED)↗
High-speed Wind-tunnel Tests of an NACA 16-009 Airfoil Having a 32.9-percent-chord Flap with an Overhang 20.7 Percent of the Flap Chord
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WIND TUNNEL TESTS - NACA - HIGH-SPEED (2')↗
Wind tunnel investigation of control-surface characteristics XXIII : a 0.25-airfoil-chord flap with tab having a chord twice the flap chord on an NACA 0009 airfoil
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TABS - DEFLECTION↗
High-speed Wind-tunnel Tests of an NACA 0009-64 Airfoil Having a 33.4-percent-chord Flap with an Overhang 20.1 Percent of the Flap Chord
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AIRFOILS - CHARACTERISTICS - EFFECT OF COMPRESSIBI↗
A comparison of the lateral controllability with flap and plug ailerons on a sweptback-wing model having full-span flaps
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AILERONS↗
Wind-tunnel Investigation of the Boundary Layer and Wake and Their Relation to Airfoil Characteristics.naca 65(sub 1)-012 Airfoil with a True Contour Flap and a Beveled-trailing-edge Flap
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Mendelsohn, Robert A↗
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↗
Investigation by the Transonic-bump Method of a 35 Degree Sweptback Semispan Model Equipped with a Flap Operated by a Series of Servovanes Located Ahead of and Geared to the Flap
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Phillips, William H↗
Wind-tunnel Investigation of Effect of Propeller Slipstreams on Aerodynamic Characteristics of a Wing Equipped with a 50-percent-chord Sliding Flap and a 30-percent-chord Slotted Flap
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Kuhn, Richard E↗
Qualitative Measurements of Relative Flap Effectiveness at Transonic Speeds on a Series of Five Thin Airfoils with 25-percent-chord Flaps and Various Amounts of Sweepback
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Crane, Harold L↗
Control effectiveness and hinge-moment measurements at a Mach number of 1.9 of a nose flap and trailing-edge flap on a highly tapered low- aspect-ratio wing
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Mitchell, Meade H , Jr↗
The Effect of Span and Deflection of Split Flaps and Leading-edge Roughness on the Longitudinal Stability and Gliding Characteristics of a 42 Degree Sweptback Wing Equipped with Leading-edge Flaps
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Pratt, George L↗
Measurements of Aerodynamic Characteristics of a 35 Degree Sweepback NACA 65-009 Airfoil Model with 1/4 Chord Flap Having 31 Percent Flap Chord Overhang Balance by the NACA Wing Flow Method
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Johnson, Harold I↗
Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.29 of an Unswept Tapered Wing of Aspect Ratio 2.67 with Leading- and Trailing-edge Flaps - Trailing-edge Flaps Deflected
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Stivers, Louis S , Jr↗