Results 301 to 310 of about 106,651 (339)

The Reduction of Main Landing Gear Noise

22nd AIAA/CEAS Aeroacoustics Conference, 2016
John Kennedy, Eleonora Neri, Gareth J. Bennett   +2 more
openaire   +1 more source

Metallurgical Failure Analysis of AA 7050 Main Landing Gear Brake Reducer for Reusable Launch Vehicle

Engineering Failure Analysis, 2022
K. Jalaja, Sushant K. Manwatkar, Rohit Kumar Gupta, S. N. Narayana Murty   +3 more
semanticscholar   +1 more source

Failure of a Main Landing Gear on a Light Airplane

2019
Abstract Initial investigation showed that a landing gear failure was the result of a hard landing with no evidence of contributory factors. The objective of reexamination was to determine whether there was any evidence of metallurgical failure.
openaire   +1 more source

Investigation of a Boeing 747 wing main landing gear trunnion failure

Engineering Failure Analysis, 2013
Abstract A loud noise was heard from the vicinity of the port wing landing gear during pushback of a Boeing 747-300 from the terminal at Sydney (Australia) airport. Inspection showed that one of the wing landing gear trunnion fork assemblies had failed. Detailed investigation revealed that the trunnion had failed by fatigue cracking.
openaire   +1 more source

Further Noise Reduction of Regional Jet Two-Wheel Main Landing Gear

Advanced Courses, 2022
Yasushi Ito, T. Takaishi, Hirokazu Shoji, Akihisa Shimada, Kensuke Hayashi, Yosuke Ueno   +5 more
semanticscholar   +1 more source

Cancer epigenetics in clinical practice

Ca-A Cancer Journal for Clinicians, 2023
Veronica Davalos, Manel Esteller
exaly  

Cancer risk among World Trade Center rescue and recovery workers: A review

Ca-A Cancer Journal for Clinicians, 2022
Paolo Boffetta, Charles B Hall, Andrew C Todd   +2 more
exaly  

Fatigue Fracture of a C130 Aircraft Main Landing Gear Wheel Flange

1992
Abstract A piece of wheel flange separated from the main landing gear wheel of a C130 aircraft as it taxied on a runway. The wheel was a 2014-T61 aluminum alloy forging and had been in service nearly 20 years. Fractographic evidence indicated that the initial crack growth was caused by high-cycle fatigue.
openaire   +1 more source

Aeroacoustic Characteristics of Main Landing Gear of High-Lift Common Research Model

AIAA AVIATION FORUM AND ASCEND 2025
Yasushi Ito, T. Takaishi, Yuta Ozawa, T. Hirai   +3 more
semanticscholar   +1 more source

Mechanism analysis of a main landing gear of transporting aircraft: A design learning perspective

, 2021
P. Kadarno, M. Barrinaya, A.O. Manurung, B. Riyandwita, S. Hastuty, Y. Rahmawan, S.A. Pradanawati, K. Widiyati, I. Putra, J. Purbolaksono   +9 more
semanticscholar   +1 more source