Application of tire dynamics to aircraft landing gear design analysis [PDF]
, 1983 The tire plays a key part in many analyses used for design of aircraft landing gear. Examples include structural design of wheels, landing gear shimmy, brake whirl, chatter and squeal, complex combination of chatter and shimmy on main landing gear (MLG ...
Black, R. J.
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Hidden Semi-Markov Models-Based Visual Perceptual State Recognition for Pilots. [PDF]
Sensors (Basel), 2023 Gao L, Wang C, Wu G.
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Validation of an Active Gear, Flexible Aircraft Take-off and Landing analysis (AGFATL) [PDF]
The results of an analytical investigation using a computer program for active gear, flexible aircraft take off and landing analysis (AGFATL) are compared with experimental data from shaker tests, drop tests, and simulated landing tests to validate the ...
Mcgehee, J. R.
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Structural response of transport airplanes in crash situations [PDF]
This report highlights the results of contractural studies of transport accident data undertaken in a joint research program sponsored by the FAA and NASA.
Caiafa, C., Thomson, R. G.
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Tesseract: Supersonic business transport [PDF]
This year, the senior level Aerospace Design class at Case Western Reserve University developed a conceptual design of a supersonic business transport. Due to the growing trade between Asia and the United States, a transpacific range has been chosen for ...
Garbinski, Gary, Reshotko, Eli
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The Flying Diamond: A joined aircraft configuration design project, volume 1 [PDF]
The results of the analysis conducted on the Joined Wing Configuration study are presented. The joined wing configuration employs a conventional fuselage and incorporates two wings joined together near their tips to form a diamond shape in both plan view
Ball, Chris +5 more
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Ditching investigation of a 1/20-scale model of the space shuttle orbiter [PDF]
The ditching characteristics of the space shuttle orbiter were examined. Tests were made with a 1/20-scale model in order to determine behavior patterns and accelerations imparted to the ditching vehicle. Ditchings were made with different configurations
Thomas, W. L.
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Design and Implementation of a New Training Flight Simulator System. [PDF]
Sensors (Basel), 2022 Wei MY, Fang SA, Liu JW.
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Technical and Economic Assessment of Span-Distributed Loading Cargo Aircraft Concepts [PDF]
A 700,000 kg (1,540,000-lb) aircraft with a cruise Mach number of 0.75 was found to be optimum for the specified mission parameters of a 272 155-kg (600,000-lb) payload, a 5560-km (3000-n.mi.) range, and an annual productivity of 113 billion revenue-ton ...
Eudaily, R. R. +5 more
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Multivariate Gas Sensor E-Nose System with PARAFAC and Machine Learning Modeling for Quantifying and Classifying the Impact of Fishing Gears. [PDF]
Sensors (Basel)Silva-Alvarado VL, Lloret J.
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