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- Aerospace Standard
Published March 17, 2006 by SAE International in United States
Downloadable datasets availableAnnotation ability available
The landing gear is a complex multi-degree of freedom dynamic system and may encounter vibration problems induced by braking action. The vibratory modes can be induced by several frictional characteristics and brake design features. These should be assessed during the design concept and verified during the development of the hardware.
This SAE Aerospace Information Report (AIR) has been prepared by a panel of the A-5A Subcommittee to present an overview of the landing gear system problems associated with aircraft brake dynamics and the approaches to the solution of these problems. In addition, facilities available for test and evaluation are presented and discussed.1
|Ground Vehicle Standard||Air Brake Actuator Test Procedure, Truck-Tractor, Bus, and Trailers|
|Ground Vehicle Standard||Brake Hydraulic Component Flow Rate Measurement for High Differential Pressure (>5 bar)|
Data Sets - Support Documents
|Unnamed Dataset 1|
|851937||Laboratory Simulation of Landing Gear Pitch-Plane Dynamics|
|AIR1489||AEROSPACE LANDING GEAR SYSTEMS TERMINOLOGY|
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