A flight evaluation of the longitudinal stability characteristics associated with the pitch-up of a swept-wing airplane in maneuvering flight at transonic speeds
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Anderson, Seth B↗
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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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Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : body of revolution
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Heitmeyer, John C↗
Wind-tunnel Investigation of the Aerodynamic Characteristics in Pitch of Wing-fuselage Combinations at High Subsonic Speeds : Aspect-ratio Series
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Kuhn, Richard E↗
Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : twisted and cambered triangular wing of aspect ratio 2 with NACA 0005-63 thickness distribution
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Heitmeyer, John 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 aerodynamic characteristics in pitch
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Robinson, Ross B↗
A Theoretical Investigation of the Effect of a Target Seeker Sensitive to Pitch Attitude on the Dynamic Stability and Response Characteristics of a Supersonic Canard Missile Configuration
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Gates, Ordway B , Jr↗
Wind-tunnel Investigation of the Aerodynamic Characteristics in Pitch of Wing-fuselage Combinations at High- Subsonic Speeds : Sweep Series
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Wiggins, James W↗
Lift, Drag and Pitching Moment of Low-aspect-ratio Wings at Subsonic and Supersonic Speeds : Plane Tapered Wing of Aspect Ratio 3.1 with 3 Percent Thick Rounded Nose Section
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Heitmeyer, John C↗
Investigation of Interference, Lift, Drag, and Pitching Moment of a Series of Rectangular Wing and Body Combinations at Mach Numbers of 1.62, 1.93,and 2.41
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Coletti, Donald E↗
The Effects of Oscillation Amplitude and Frequency on the Experimental Damping in Pitch of a Triangular Wing Having an Aspect Ratio of 4
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Beam, Benjamin H↗
Preliminary Investigation of the Low-amplitude Damping in Pitch of Tailless Delta- and Swept-wing Configurations at Mach Numbers from 0.7 to 1.35
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D'Aiutolo, Charles T↗
Summary of pitch-damping derivatives of complete airplane and missile configurations as measured in flight at transonic and supersonic speeds
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Gillis, Clarence L↗
The Low-speed Lift and Pitching Moment Characteristics of a 45 Degree Sweptback Wing of Aspect Ratio 8 with and Without High-lift and Stall-control Devices as Determined from Pressure Distribution at a Reynolds Number of 4.0 x 10(exp 6)
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Bollech, Thomas V↗
Lift, drag and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : comparison of three wings of aspect ratio 2 of rectangular, swept-back and triangular plan form, including effects of thickness distribution
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Hightower, Ronald C↗
Flight investigation of a supersonic canard missile equipped with an auxiliary damping-in-pitch control system
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Moul, Martin T↗
Damping in pitch of low-aspect-ratio wings at subsonic and supersonic speeds
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Tobak, Murray↗
Moment of inertia and damping of fluid in tanks undergoing pitching oscillations
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Widmayer, Edward, Jr↗
Wind-tunnel Investigation of the Aerodynamic Characteristics in Pitch of Wing-fuselage Combinations at High Subsonic Speeds : Taper-ratio Series
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King, Thomas J , Jr↗