Experimental Investigation of the Effects of Sweepback on the Flutter of a Uniform Cantilever Wing with a Variably Located Concentrated Mass
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Nelson, Herbert C↗
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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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Temperature Survey of the Wake of Two Closely Located Parallel Jets
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Sloop, John L↗
Investigation of Effect of Span and Spanwise Location of Plain and Stepped Spoiler Ailerons on Lateral Control Characteristics of a Wing with Leading Edge Swept Back 51.3 Degrees
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Fischel, Jack↗
Experimental investigation of the effects of root restraint on the flutter of a sweptback, uniform, cantilever wing with a variably located concentrated mass
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Tomassoni, John E↗
Effect of Wing-tank Location on the Drag and Trim of a Swept-wing Model as Measured in Flight at Transonic Speeds
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Welsh, Clement J↗
The effect of aileron span and spanwise location on the low-speed lateral control characteristics of an untapered wing of aspect ratio 2.09 and 45 degree sweepback
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Naeseth, Rodger L↗
Effects of Varying the Size and Location of Trailing-edge Flap-type Controls on the Aerodynamic Characteristics of a Unswept Wing at a Mach Number of 1.9
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Mitchell, Meade H , Jr↗
The Effect of Spanwise Aileron Location on the Rolling Effectiveness of Wings with 0 Degree and 45 Degree Sweep at Subsonic, Transonic, and Supersonic Speeds
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Strass, H Kurt↗
Effects of plain and step spoiler location and projection on the lateral control characteristics of a plain and flapped 42 degree sweptback wing at a Reynolds number of 6.8 x 10(exp 6)
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Bollech, Thomas V↗
Effects of Spoiler on Airfoil Pressure Distribution and Effects of Size and Location of Spoilers on the Aerodynamic Characteristics of a Tapered Unswept Wing of Aspect Ratio 2.5 at a Mach Number of 1.90
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Conner, D William↗
Wind-tunnel Investigation at Subsonic and Low Transonic Speeds of the Effects of Aileron Span and Spanwise Location on the Rolling Characteristics of a Test Vehicle with Three Untapered 45 Degree Sweptback Wings
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Johnson, Harold S↗
An investigation of the effect of vertical-fin location and area on low-speed lateral stability derivatives of a semitailless airplane model
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Fisher, Lewis R↗
Flight Investigation at Mach Numbers from 0.8 to 1.5 of the Drag of a Canopy Located at Two Positions on a Parabolic Body of Revolution
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Welsh, Clement J↗
Transonic Flight Tests to Determine Zero-lift Drag and Pressure Recovery of Nacelles Located at the Wing Tips on a 45 Degree Sweptback Wing and Body Combination
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Hoffman, Sherwood↗
Some effects of spanwise aileron location and wing structural rigidity on the rolling effectiveness of 0.3-chord flap-type ailerons on a tapered wing having 63 degrees sweepback at the leading edge and NACA 64A005 airfoil sections
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Strass, H Kurt↗
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↗
Full-scale Wind-tunnel Investigation of the Effects of Wing Modifications and Horizontal-tail Location on the Low-speed Static Longitudinal Characteristics of a 35 Degree Swept-wing Airplane
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Maki, Ralph L↗
Effect of Vertical Location of a Horizontal Tail on the Static Longitudinal Stability Characteristics of a 45 Degree Sweptback-wing-fuselage Combination of Aspect Ratio 8 at a Reynolds Number of 4.0 x 10(exp 6)
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Salmi, Reino J↗