A simplified mathematical model for calculating aerodynamic loading and downwash for midwing wing-fuselage combinations with wings of arbitrary plan form
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Zlotnick, Martin↗
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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 at High Subsonic Speeds of the Static Longitudinal and Static Lateral Stability Characteristics of a Wing-fuselage Combination Having a Triangular Wing of Aspect Ratio 2.31 and an NACA 65A003 Airfoil
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Wiggins, James W↗
Investigation of wing flutter at transonic speeds for six systematically varied wing plan forms
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Jones, George W , Jr↗
Wing Loads on the Bell X-1 Research Airplane (10 Percent Thick Wing) as Determined by Pressure-distribution Measurements in Flight at Subsonic and Transonic Speeds
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Knapp, Ronald J↗
Wind-tunnel investigation of the aerodynamic characteristics in pitch and sideslip at high subsonic speeds of a wing fuselage combination having a triangular wing of aspect ratio 4
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Fournier, Paul G↗
The Effects of Leading-edge Extensions, a Trailing-edge Extension, and a Fence on the Static Longitudinal Stability of a Wing-fuselage-tail Combination Having a Wing with 35 Degrees of Sweepback and an Aspect Ratio of 4.5
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Selan, Ralph↗
Transonic Flight Tests to Determine Zero-lift Drag and Pressure Recovery of Nacelles Located at the Wing Root on a 45 Degree Sweptback Wing and Body Configuration
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Hoffman, Sherwood↗
A transonic wind-tunnel investigation of the effects of body indentation on the aerodynamic characteristics of an approximate-delta-wing-body configuration, and a comparison with a wing of reversed plan form
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Williams, Claude V↗
Free-flight Longitudinal-stability Investigation Including Some Effects of Wing Elasticity from Mach Numbers of 0.85 to 1.34 of a Tailless Missile Configuration Having a 45 Degree Sweptback Wing of Aspect Ratio 5.5
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Arbic, Richard G↗
Free-fall Measurements of the Effects of Wing-body Interference on the Transonic Drag Characteristics of Swept-wing-slender-body Configurations
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Kurbjun, Max C↗
Investigation of the Effects of Wing and Tail Modifications on the Low-speed Stability Characteristics of a Model Having a Thin 40 Degree Swept Wing of Aspect Ratio 3.5
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Weil, Joseph↗
Flight Measurement of Aerodynamic Loads and Moments on an External Store Mounted Under the Wing of a Swept-wing Fighter-type Airplane
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O'Bryan, Thomas C↗
Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the static lateral stability characteris
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Hamilton, Clyde V↗
Comparison of the Aerodynamic Characteristics at Transonic Speeds of a Plane Wing and a Cambered and Twisted Wing, Both Having 45 Degrees of Sweepback and an Aspect Ratio of 6
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Holdaway, George H↗
Measurements of fluctuating pressures on the wings and body of a sweptback wing-body combination in the Langley 16-foot transonic tunnel
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Habel, Louis W↗
Wind-tunnel Investigation of the Vortex Wake and Downwash Field Behind Triangular Wings and Wing-body Combinations at Supersonic Speeds
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Spahr, J Richard↗
An Analysis of the Tracking Performances of Two Straight-wing and Two Swept-wing Fighter Airplanes with Fixed Sights in a Standardized Test Maneuver
Standard air-to-air-gunnery tracking runs were conducted with F-51H, F8F-1, F-86A, and F-86E airplanes equipped with fixed gunsights. The tracking performances were documented over the normal operating range of altitude, Mach number, and normal acceleration factor for each airplane. The sources of error were studied by statistical analyses of the aim wander.
CONTROL, LATERAL↗
Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the static lateral stability characteris
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Hilton, John H , Jr↗