Investigation of Mutual Interference Effects of Several Vertical-tail-fuselage Configuration in Sideslip
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Michael, William H , Jr↗
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Results for “FUSELAGE”
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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Directional Stability Characteristics of Two Types of Tandem Helicopter Fuselage Models
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Williams, James L↗
Surveys of the Flow Fields at the Propeller Planes of Six 40 Degree Sweptback Wing-fuselage-nacelle Combinations
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Rogallo, Vernon L↗
Static stability of fuselages having a relatively flat cross section
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Bates, William R↗
Some effects of fuselage flexibility on longitudinal stability and control
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Klawans, Bernard B↗
Experimental investigation at low speed of effects of fuselage cross section on static longitudinal and lateral stability characteristics of models having 0 and 45 degrees sweptback surfaces
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Letko, William↗
An analysis of estimated and experimental transonic downwash characteristics as affected by plan form and thickness for wing and wing-fuselage configurations
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Weil, Joseph↗
Experimental Steady-state Yawing Derivatives of a 60 Degree Delta-wing Model as Affected by Changes in Vertical Position of the Wing and in Ratio of Fuselage Diameter to Wing Span
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Jaquet, Byron M↗
Experimental Investigation at Low Speed of the Effects of Wing Position on the Static Stability of Models Having Fuselages of Various Cross Section and Unswept and 45 Degrees Sweptback Surfaces
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Letko, William↗
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↗
Investigation at Low Speeds of Deflectors and Spoilers as Gust Alleviators on a Model of the Bell X-5 Airplane with 35 Degree Swept Wings and on a High-aspect-ratio 35 Degree Swept-wing-fuselage Model
Results of an investigation at low speeds to determine the gust-alleviation capabilities (reduction in lift-curve slope) of spoilers and deflectors on a 35 degree swept-wing model of high aspect ratio and on a 1/4-scale model of the X-5 airplane with 35 degree swept wings indicate that deflector and spoiler-deflector types of controls can be designed to provide considerable gust alleviation for a swept-wing airplane while still maintaining stability and control.
CONTROLS, SPOILER - COMPLETE WINGS↗
Weight-strength studies of structures representative of fuselage construction
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Peterson, James P↗
Some aspects of fail-safe design of pressurized fuselages
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Kuhn, Paul↗
Wind-tunnel Investigation of the Static Lateral Stability Characteristics of Wind-fuselage Combinations at High Subsonic Speeds : Taper-ratio Series
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Wiggins, James W↗
A Fuselage Addition to Increase Drag-rise Mach Number of Subsonic Airplanes at Lifting Conditions
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Whitcomb, Richard T↗
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↗
Free-flight Investigation to Determine the Drag of Flat- and Vee- Windshield Canopies on a Parabolic Fuselage with and Without Transonic Indentation Between Mach Numbers of 0.75 and 1.35
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Kouyoumjian, Walter L↗
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↗