Analysis Of Landing Gear Impact Including The Effects Of Wheel Spinup
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Author | : Charles William Coale |
Publisher | : |
Total Pages | : 310 |
Release | : 1953 |
Genre | : Airplanes |
ISBN | : |
Download Analysis of Landing Gear Impact Including the Effects of Wheel Spinup Book in PDF, Epub and Kindle
Author | : Walther Boccius |
Publisher | : |
Total Pages | : 70 |
Release | : 1948 |
Genre | : Airplanes |
ISBN | : |
Download Loads on and Behavior of Landing Gears During the First Phase of the Landing Impact Book in PDF, Epub and Kindle
Author | : W. Flügge |
Publisher | : |
Total Pages | : 107 |
Release | : 1954 |
Genre | : Airplanes |
ISBN | : |
Download The Influence of Wheel Spin-up on Landing-gear Impact Book in PDF, Epub and Kindle
The possibilities of an eccentric wheel and of an inclined shock strut have been considered. In both cases the computation is rather involved. The binding of the piston due to ovalization of the shock strut cylinder does not seem to present a serious problem.
Author | : Norman S. Silsby |
Publisher | : |
Total Pages | : 32 |
Release | : 1962 |
Genre | : Airplanes |
ISBN | : |
Download An Analytical Study of Effects of Some Airplane and Landing-gear Factors on the Response to Runway Roughness with Applicationis to Supersonic Transports Book in PDF, Epub and Kindle
Author | : Benjamin Milwitzky |
Publisher | : |
Total Pages | : 348 |
Release | : 1955 |
Genre | : Aeronautics |
ISBN | : |
Download Theoretical and Analog Studies of the Effects of Nonlinear Stability Derivatives on the Longitudinal Motions of an Aircraft in Response to Step Control Deflections and to the Influence of Proportional Automatic Control Book in PDF, Epub and Kindle
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 44 |
Release | : 1955 |
Genre | : Aeronautics |
ISBN | : |
Download Report Book in PDF, Epub and Kindle
Author | : Jocelyn I. Pritchard |
Publisher | : |
Total Pages | : 22 |
Release | : 1999 |
Genre | : Aerodynamics |
ISBN | : |
Download An Overview of Landing Gear Dynamics Book in PDF, Epub and Kindle
On of the problems facing the aircraft community is landing gear dynamics, especially shimmy and brake-induced vibration. Shimmy and brake-induced vibrations can lead to accidents due to excessive wear and shortened life of gear parts and contribute to pilot and passenger discomfort. To increase understanding of these problems, a literature survey was performed. The major focus is on work from the last ten years. Some older publications are included to understand the longevity of the problem and the background from earlier researchers. The literature survey includes analyses, testing, modeling, and simulation of aircraft landing gear; and experimental validation and characterization of shimmy and brake-induced vibration of aircraft landing gear. The paper presents an overview of the problem, background information, and a history of landing gear dynamics problems and solutions. Based on the survey an assessment and recommendations of the most critically needed enhancements to the state of the art will be presented. The status of Langley work contributing to this activity will be given.
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 874 |
Release | : 1954 |
Genre | : Aeronautics |
ISBN | : |
Download Technical Note - National Advisory Committee for Aeronautics Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 490 |
Release | : |
Genre | : Aeronautics |
ISBN | : |
Download Technical Note Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 86 |
Release | : 1982 |
Genre | : Aircraft |
ISBN | : |
Download A Study of Analytic Modeling Techniques for Landing Gear Dynamics Book in PDF, Epub and Kindle
The ability to accurately predict the dynamic response of an aircraft while it is operating in the taxi mode depends, in part on the correct modeling of the dynamic characteristics of the landing gear system. Traditionally, landing gear have been designed to absorb landing impact ('shock absorber') and their characteristics during periodic, oscillatory response ('spring') have been considered as secondary. With the increased emphasis on the rough or damaged field taxi operation, there is a requirement to determine the best methods for modeling the gear system. This report documents a brief review of the state of the art of gear modeling. A study was then conducted to evaluate important model parameters, using a simple cantilevered gear computer simulation. Also included is the development of a technique for the experimental determination of important gear system parameters. (Author).