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↗
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Results for “STABILITY, LONGITUDINAL - STATIC”
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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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↗
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↗
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↗
Effects of wing inboard plan-form modifications on lift, drag, and longitudinal stability at Mach numbers from 1.0 to 2.3 of a rocket-propelled free-flight model with a 52.5 degree sweptback wing of aspect ratio 3
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Henning, Allen B↗
Longitudinal Stability Investigation of a Vertical-take-off-and-landing Airplane Configuration with Simulated Jet Intake and Exhaust at Mach Numbers of 1.61 and 2.01
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Lord, Douglas R↗
Dynamic Longitudinal Stability Characteristics of a Swept-wing Fighter-type Airplane at Mach Numbers Between 0.36 and 1.45
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Wolowicz, Chester H↗
Longitudinal Stability and Control Characteristics at Mach Numbers of 1.41 and 2.01 of a 67 Degree Swept-wing Airplane Configuration with Canard Control Surfaces
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Spearman, M Leroy↗
Transonic Wind-tunnel Investigation of the Effect of Horizontal Tail on Longitudinal Stability of Two 60 Degree Sweptback-wing--body Configurations with Aspect Ratios of 2.67 and 4.00
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Brooks, Joseph D↗
Free-flight Investigation of Jet Effects at Low Supersonic Mach Numbers on a Fighter-type Configuration Employing a Tail-boom Assembly : Longitudinal Stability and Trim
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Jackson, Bruce G↗
The problem of longitudinal stability and control at high speeds
In high-speed dives many airplanes exhibit a dangerous tendency to continue diving in spite of the application of large control forces. Wind-tunnel tests have confirmed that these difficulties are not peculiar to any particular configuration, so that the problem is of interest to all designers of high-speed airplanes. The purpose of this report is to acquaint designers with the cause of difficulties and with the means now known for their alleviation.
Hood, Manley J↗
Effect of Tilt of the Propeller Axis on the Longitudinal-stability Characteristics of Single-Engine Airplanes
Report presents the results of tests of a model of a single-engine airplane with two different tilts of the propeller axis. The results indicate that on a typical design a 5 degree downward tilt of the propeller axis will considerably reduce the destabilization effects of power. A comparison of the experimental results with those computed by use of existing theory is included. A comparison of the experimental results with those computed by use of existing theory is included. It is shown that the results can be predicted with an accuracy acceptable for preliminary design purposes, particularly at the higher powers where the effects are of significant magnitude.
Goett, Harry J↗
An analytical investigation of the effects of elevator-fabric distortion on the longitudinal stability and control of an airplane
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STABILITY & CONTROL↗
Some theoretical considerations of longitudinal stability in power-on flight with special reference to wind-tunnel testing
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Donlan, Charles J↗