Contribution of the Wing Panels to the Forces and Moments of Supersonic Wing-body Combinations at Combined Angles
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Spahr, J Richard↗
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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 of Lateral Control near the Stall Flight Tests with High-wing and Low-wing Monoplanes of Various Configurations
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Weick, Fred E↗
A correlation of results of a flight investigation with results of an analytical study of effects of wing flexibility on wing strains due to gusts
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Shufflebarger, C C↗
Experimental Measurements of the Effects of Airplane Motions on Wing and Tail Angles of Attack of a Swept-wing Bomber in Rough Air
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Engel, Jerome N↗
An Evaluation of the Effects of Flexibility on Wing Strains in Rough Air for a Large Swept-wing Airplane by Means of Experimentally Determined Frequency-response Functions with an Assessment of Random-process Techniques Employed
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Coleman, Thomas L↗
Effects of Frequency and Amplitude on the Yawing Derivatives of Triangular, Swept, and Unswept Wings and of a Triangular-wing-fuselage Combination with and Without a Triangular Tail Performing Sinusoidal Yawing Oscillations
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Letko, William↗
Idealized Wings and Wing-bodies at a Mach Number of 3
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Katzen, Elliott D↗
Longitudinal Stability and Control Characteristics of a Semispan Airplane Model with a Sweptback Wing and Tail from Tests at Transonic Speeds by the NACA Wing-flow Method
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Sawyer, Richard H↗
Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Investigation of a Large-scale Model at Low Speed
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Mccormack, Gerald M↗
Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel I : Characteristics of a Plain Wing
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Johnson, Ben H , Jr↗
Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel II : The Effect of Constant-chord Leading- and Trailing-edge Flaps on the Low-speed Characteristics of the Wing
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Bandettini, Angelo↗
Investigation of Wing Characteristics at a Mach Number of 1.53 III : Unswept Wings of Differing Aspect Ratio and Taper Ratio
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Nielsen, Jack N↗
Effect of Wing Sweep, Taper, and Thickness Ratio on the Transonic Drag Characteristics of Wing-body Combinations
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Thompson, Jim Rogers↗
Some Pressure-distribution Measurements on a Swept-wing at Transonic Speeds by the NACA Wing-flow Method
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Johnston, J Ford↗
Comparison of the Transonic Drag Characteristics of Two Wing-body Combinations Differing Only in the Location of the 45 Degree Sweptback Wing
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Mathews, Charles W↗
Investigation of Wing Characteristics at a Mach Number of 1.53 I : Triangular Wings of Aspect Ratio 2
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Vincenti, Walter G↗
Air-flow Behavior over the Wing of an XP-51 Airplane as Indicated by Wing-surface Tufts at Subcritical and Supercritical Speeds
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Beeler, De E↗
Tests of a Triangular Wing of Aspect Ratio 2 in the Ames 12-foot Pressure Wind Tunnel I : the Effect of Reynolds Number and Mach Number on the Aerodynamic Characteristics of the Wing with Flap Undeflected
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Edwards, George G↗