Effects of Reynolds number and leading-edge shape on the low-speed longitudinal stability of a 6-percent-thick 45 degree sweptback wing
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Schneider, William 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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Lift, drag, and static longitudinal stability characteristics of configurations consisting of three triangular wing panels and a body of equal length at Mach numbers from 3.00 to 6.28
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Savin, Raymond C↗
Effect of fuselage air brakes on the longitudinal stability characteristics of a swept wing fighter model at transonic speeds
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Arabian, Donald D↗
A transonic investigation of the static longitudinal-stability characteristics of a 45 degree sweptback wing-fuselage combination with and without horizontal tail
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Critzos, Chris C↗
Results of Rocket Model Test of an Airplane Configuration Having an Arrow Wing and Slender Flat-sided Fuselage : Lift, Drag, Longitudinal Stability, Lateral Force, and Jet Effects at Mach Numbers Between 1.0 and 2.3
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Peck, Robert F↗
Effects of leading-edge radius on the longitudinal stability characteristics of two 60 degree sweptback wings at high Reynolds numbers
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Schneider, William C↗
Longitudinal Stability Characteristics of a Simple Infrared Homing Missile Configuration at Mach Numbers of 0.7 to 1.4
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Brown, Clarence, A , jr↗
Large-scale low-speed wind-tunnel tests of a model having a 60 degree delta horizontal canard control surface and wing to obtain static-longitudinal-stability and canard surface hinge-moment data
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Burrows, Dale L↗
A Simulator Study of Some Longitudinal Stability and Control Problems of a Piloted Aircraft in Flights to Extreme Altitude and High Speed
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Matthews, Howard F↗
Combined Effects of Wing Taper Ratio and Low Horizontal-Tail Position on Longitudinal Stability of a 45 Degree Sweptback Wing-Body Combination at Transonic Speeds
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Spooner, Stanley H↗
An analytical study of the effects of increasing fin chord on the lift and longitudinal stability characteristics of constant-span fin-body combinations of fineness ratio 14
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English, Roland D↗
Investigation at high subsonic speeds of the effects of various horizontal fuselage forebody fins on the directional and longitudinal stability of a complete model having a 45 degree sweptback wing
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Sleeman, William C , Jr↗
Longitudinal Stability Characteristics of the Convair YF-102 Airplane Determined from Flight Tests
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Andrews, William H↗
Investigation of static longitudinal stability characteristics at transonic speeds of 30 degree sweptback wing in wing-body configuration with and without horizontal tail
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Willis, Conrad M↗
Exploratory Investigation of the Effect of Wing Slots and Leading-edge Slats on the Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing-fuselage Configuration
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Critzos, Chris C↗
Investigation of the Low-speed Performance and Static Longitudinal Stability and Control Characteristics of a 60 Degree Delta-wing--body--tail Combination with Blowing over Trailing-edge Flaps
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Scallion, William I↗
Effects of Wing Warp on the Lift, Drag, and Static Longitudinal Stability Characteristics of an Aircraft Configuration Having an Arrow Wing of Aspect Ratio 1.86 at Mach Numbers from 1.1 to 1.7
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Gillespie, Warren, Jr↗
Wind-tunnel investigation of static lateral and longitudinal stability characteristics of a 1/62-scale model of the X-1E airplane at combined angles of attack and sideslip at supersonic speeds
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Henderson, Arthur, Jr↗