Lift and Moment Characteristics at Subsonic Mach Numbers of Four 10-percent-thick Airfoil Sections of Varying Trailing-edge Thickness
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Summers, James L↗
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Effects on the Snaking Oscillation of the Bell X-1 Airplane of a Trailing-Edge Bulb on the Rudder
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Drake, Hubert M↗
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 : Flaps Deflected in Combination
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Stivers, Louis S , Jr↗
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 - Leading-edge Flaps Deflected
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Stivers, Louis S , Jr↗
Experimental downwash and wake characteristics at subsonic and supersonic Mach numbers behind an unswept, tapered wing, of aspect ratio 2.67 with leading-and trailing-edge flaps
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Stivers, Louis S , Jr↗
Experimental investigation of air-cooled turbine blades in turbojet engine VI : conduction and film cooling of leading and trailing edges of rotor blades
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Arne, Vernon L↗
Investigation at Supersonic Speeds of Some of the Factors Affecting the Flow over a Rectangular Wing with Symmetrical Circular-arc Section and 30-percent-chord Trailing-edge Flap
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Czarnecki, K R↗
Experimental investigation of air-cooled turbine blades in turbojet engine V : rotor blades with split trailing edges
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Smith, Gordon T↗
Free-flight Measurements at Mach Numbers from 0.7 to 1.6 of Some Effects of Airfoil-thickness Distribution and Trailing-edge Angle on Aileron Rolling Effectiveness and Drag for Wings with 0 and 45 Degrees Sweepback
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Fields, E M↗
Theoretical analyses to determine unbalanced trailing-edge controls having minimum hinge moments due to deflection at supersonic speeds
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Goin, Kennith L↗
Comparison of Semispan and Full-span Tests of a 47.5 Degrees Sweptback Wing with Symmetrical Circular-arc Sections and Having Drooped-nose Flaps, Trailing-edge Flaps, and Ailerons
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Lipson, Stanley↗
Effects on Control Effectiveness of Systematically Varying the Size and Location of Trailing-edge Flaps on a 45 Degrees Sweptback Wing at a Mach Number of 1.9
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Jacobsen, Carl R↗
Effect of section thickness and trailing-edge radius on the performance of NACA 65-series compressor blades in cascade at low speeds
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Herrig, L Joseph↗
Effects of three types of blunt trailing edges on the aerodynamic characteristics of a plane tapered wing of aspect ratio 3.1, with a 3-percent- thick biconvex section
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Dugan, Duane W↗
The Effects at Transonic Speeds of Thickening the Trailing Edge of a Wing with a 4-percent-thick Circular-arc Airfoil
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Cleary, Joseph W↗
Effect of Trailing Edge Thickness on Lift at Supersonic Velocities
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Chapman, Dean R↗
Effects of Plan Form, Airfoil Section, and Angle of Attack on the Pressures Along the Base of Blunt-trailing-edge Wings at Mach Numbers of 1.41, 1.62, and 1.96
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Goin, Kennith L↗
Investigation at Low Speed of the Downwash, Sidewash, and Wake Characteristics Behind a Large-scale Triangular Wing, Including the Effects of Yaw, Full-span Trailing-edge Flaps, and Two Leading- Edge Modifications
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Whittle, Edward F JR↗