Results 261 to 270 of about 7,860,213 (302)

Aerodynamic Characteristics of the Aircraft Main Landing Gear System

Advances in Engineering Technology Research
As one of the most structurally complex and load-bearing components, the main landing gear (MLG) system experiences substantial aerodynamic loads during aircraft takeoff, landing, and retraction/extension sequences. Its aerodynamic characteristics profoundly impact the reliability of the retraction/extension mechanism and the structural fatigue life of
Leyao Lin, Xi Wang, Bingzhi Chen, Chen Wang, Guang Feng   +4 more
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Rotational Drop-Testing of Airplane Main Landing Gear

Journal of Fluids Engineering, 1946
Abstract The immediate physical objectives of drop-testing are presented, together with a general method for conducting rotational tests that have proper contact velocity and energy relationships coincidental with the absence of undesirable dynamic reactions at the pivot axis.
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The noise generation by a main landing gear door [PDF]

, 2016
Experimental measurements and numerical simulations were conducted on a simplified main landing gear model that consists of a leg-door, and a main strut in a parallel configuration. The effects of varying the leg-door angle of attack, and the gap distance between the two elements, were initially studied by two-dimensional and low-order numerical ...
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CF-105 service data. Main landing gear

1956
digitized filename: Box-06\15825331_main_landing_gear ...
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Prediction of fatigue life of a main landing gear

AIP Conference Proceedings, 2023
Utkarsh Verma, Amit Kumar Soni, Vijay Gautam   +2 more
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Arrow 1 service data. Main landing gear

1955
Corporate author and publisher are assumed to be "Avro Aircraft Limited (Canada)" by the National Research Council of Canada.
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Shimmy of Aircraft Main Landing Gears

2000
Mechanical Maritime and Materials ...
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Design of main landing gear of jet trainer

1954
Thesis (B.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1954. ; MIT copy bound with: An investigation and comparison of the subsonic aerodynamic characteristics of the swept and crescent wing configurations / William Strike & George Perrone [1954] ; Includes bibliographical references (leaf 38). ; by Milton Toorans. ; B.
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The Reduction of Main Landing Gear Noise

22nd AIAA/CEAS Aeroacoustics Conference, 2016
John Kennedy, Eleonora Neri, Gareth J. Bennett   +2 more
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Fatigue Crack Growth in Aircraft Main Landing Gear Wheels

1988
Fracture analysis of aircraft landing gear wheels under service-simulated operating loads using various fatigue crack growth characterization techniques is presented. Baseline constants for the wheel forging alloy 2014-T6 aluminum are established. The stress-intensity factors for a two-dimensional surface crack are developed using a proposed load model
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