Low-speed Wind-tunnel Investigation of Various Plain-spoiler Configurations for Lateral Control on a 42 Degree Sweptback Wing
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WINGS, SWEPTBACK - CHARACTERISTICS↗
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Effects of Mach Number and Reynolds Number on the Maximum Lift Coefficient of a Wing of NACA 230-series Airfoil Sections
Wing was tested with full-span, partial-span, or split flaps deflected 60 Degrees and without flaps. Chordwise pressure-distribution measurements were made for all flap configurations.. Peak values of maximum lift coefficient were obtained at relatively low free-stream Mach numbers and, before critical Mach number was reached, were almost entirely dependent on Reynolds Number. Lift coefficient increased by increasing Mach number or deflecting flaps while critical pressure coefficient was reached at lower free-stream Mach numbers.
LIFT COEFFICIENTS - AIRFOILS - NACA 230↗
Wind-tunnel Investigation at Low Speed of the Lateral Control Characteristics of Ailerons Having Three Spans and Three Trailing-edge Angles on a Semispan Wing Model
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WINGS, TAPERED - CHARACTERISTICS↗
Effects of antispin fillets and dorsal fins on the spin and recovery characteristics of airplanes as determined from free-spinning-tunnel tests
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WIND TUNNEL TESTS - NACA - FREE-SPINNING (20') WOR↗
Review of flight tests of NACA C and D cowlings on the XP-42 airplane
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PRESSURE DISTRIBUTION - ENGINES↗
Two-dimensional Wind-tunnel Investigation of the NACA 64(sub 1)-012 Airfoil Equipped with Two Types of Leading-edge Flap
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AIRFOILS - NACA 641-012 - CHAR ,MOMENTS & ORDINATE↗
Experimental Determination of the Damping in Roll and Aileron Rolling Effectiveness of Three Wings Having 2 Degree, 42 Degree and 62 Degree Sweepback
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WORK CARRIED ON AT LAL↗
Comparison Between the Measured and Theoretical Span Loadings on a Moderately Swept-forward and a Moderately Swept-back Semispan Wing
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PRESSURE DISTRIBUTION - WINGS, SWEPTBACK & SWEPTFO↗
High-speed Wind-tunnel Investigation of an NACA 65-210 Semispan Wing Equipped with Plug and Retractable Ailerons and a Full-span Slotted Flap
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AILERONS, RETRACTABLE↗
Investigation of Effects of Geometric Dihedral on Low-speed Static Stability and Yawing Characteristics of an Untapered 45 Degree Sweptback-wing Model of Aspect Ratio 2.61
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AIRFOILS - NACA 0012↗
Investigation at Low Speeds of the Effect of Aspect Ratio and Sweep on Static and Yawing Stability Derivatives of Untapered Wings
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ROLLING, PITCHING & YAWING MOMENTS - WINGS↗
Effect of Taper Ratio on Low-speed Static and Yawing Stability Derivatives of 45 Degree Sweptback Wings with Aspect Ratio of 2.61
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WIND TUNNEL TESTS - NACA - STABILITY WORK CARRIED ↗
Estimation of effectiveness of flap-type controls on sweptback wings
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ROLLING & PITCHING MOMENTS - WINGS, SWEPTBACK↗
Experimental and Calculated Characteristics of Several High-aspect-ratio Tapered Wings Incorporating NACA 44-series, 230-series, and Low-drag 64- Series Airfoil Sections
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STALLING - TAPERED WINGS↗
Divergence of swept wings
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WINGS, TAPERED↗
Effect of length-beam ratio on aerodynamic characteristics of flying-boat hulls without wing interference
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HULLS - NACA 203 - CHARACTERISTICS↗
Chordwise Pressure Distributions on a 12-foot-span Wing of NACA 66-series Airfoil Sections up to a Mach Number of 0.60
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AIRFOILS - NACA 66-SERIES - ORDINATES - LOW-DRAG↗
The Effects of Compressibility on the Lift, Pressure, and Load Characteristics of a Tapered Wing of NACA 66-series Airfoil Sections
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AIRFOILS - NACA 66-SERIES - ORDINATES - LOW-DRAG↗