Measurement of Aircraft Tire Mechanical Properties Used in Shimmy Analysys By Means Scale Models PDF Download
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Author: G. H. Nybakken
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
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Author: G. H. Nybakken
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
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Book Description
Author: G. H. Nybakken
Publisher:
ISBN:
Category :
Languages : en
Pages : 35
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Author: Samuel Kelly Clark
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 90
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Book Description
A theoretical and experimental investigation of the feasibility of determining the mechanical properties of aircraft tires from small-scale model tires was accomplished. The theoretical results indicate that the macroscopic static and dynamic mechanical properties of aircraft tires can be accurately determined from the scale model tires although the microscopic and thermal properties of aircraft tires can not. The experimental investigation was conducted on a scale model of a 40 x 12, 14 ply rated, type 7 aircraft tire with a scaling factor of 8.65. The experimental results indicate that the scale model tire exhibited the same static mechanical properties as the prototype tire when compared on a dimensionless basis. The structural modeling concept discussed in this report is believed to be exact for mechanical properties of aircraft tires under static, rolling, and transient conditions.
Author: S.K. CLARK
Publisher:
ISBN:
Category :
Languages : en
Pages : 68
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Author: Robert H. Daugherty
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 108
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Book Description
Author: Robert F. Smiley
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 176
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Book Description
A study is presented of pneumatic tires which are of interest to aircraft designers. The principal topics discussed are tire vertical-force-deflection characteristics; lateral, fore-and-aft, and torsional spring constants; footprint-area properties; relaxation lengths; rolling radius; cornering force, cornering power, self-alining torque, and pneumatic caster for yawed rolling conditions; effects of wheel tilt; and tire radial growth under the influence of centrifugal forces.
Author: Pamela A. Davis
Publisher:
ISBN:
Category : Damping (Mechanics)
Languages : en
Pages : 48
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Author: United States. National Bureau of Standards. Office of Vehicle Systems Research
Publisher:
ISBN:
Category : Motor vehicles
Languages : en
Pages : 228
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Author: Robert Kyle Schmidt
Publisher: SAE International
ISBN: 0768082188
Category : Technology & Engineering
Languages : en
Pages : 138
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Book Description
The aircraft landing gear system is relatively unique on board an aircraft—it is both structure and machine, supporting the aircraft on the ground, yet providing functions such as energy absorption during landing, retraction, steering, and braking. Advances in Aircraft Landing Gear is a collection of eleven hand-picked technical papers focusing on the significant advancements that have occurred in this field concerning numeric modeling, electric actuation, and composite materials. Additionally, papers discussing self-powered landing gear and more electrical overall aircraft architectures have been included. The content of Advances in Aircraft Landing Gear is divided into two sections: Analysis and Design Methods; and Electric Actuation, Control, and Taxi. For those looking for more information on aircraft landing gears, the SAE A-5 committee (the Aerospace Landing Gear Systems Committee), which meets twice a year, serves as a useful forum for discussion on landing gear issues and development. A current listing of documents produced and maintained by this committee appears in the appendix.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 52
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