Works matching DE "AIRPLANE landing gear"
Results: 30
Adaptive landing gear: Optimum control strategy and potential for improvement.
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- Shock & Vibration, 2009, v. 16, n. 2, p. 175
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Identification of a non-linear landing gear model using nature-inspired optimization.
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- Shock & Vibration, 2008, p. 257, doi. 10.1155/2008/246271
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Heave-Pitch-Roll Dynamics of Flexible Vehicle in Variable VelocityRun.
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- Vehicle System Dynamics, 2000, v. 33, n. 1, p. 1, doi. 10.1076/0042-3114(200001)33:1;1-5;FT001
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Discharge coefficient calculation method of landing gear shock absorber and its influence on drop dynamics.
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- Journal of Vibroengineering, 2018, v. 20, n. 7, p. 2550, doi. 10.21595/jve.2018.19049
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1347. Landing dynamic simulation of aircraft landing gear with multi-struts.
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- Journal of Vibroengineering, 2014, v. 16, n. 5, p. 2494
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Raymor Aerospace Receives AS 9100 Certification.
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- Advanced Materials & Processes, 2007, v. 165, n. 8, p. 77
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Landing Gear Failure Analysis.
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- Advanced Materials & Processes, 2006, v. 164, n. 5, p. 39
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Advanced ausbay quenching.
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- Advanced Materials & Processes, 1998, v. 154, n. 4, p. 191
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Resolving applied-mechanics problems in creating Antonov transport aircraft.
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- International Applied Mechanics, 2006, v. 42, n. 10, p. 1085, doi. 10.1007/s10778-006-0180-2
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Critical shimmy speed of nonswiveling landing-gear wheels subject to lateral loading.
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- International Applied Mechanics, 2006, v. 42, n. 9, p. 1077, doi. 10.1007/s10778-006-0179-8
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Mechanical phenomena in ground run of an aircraft with near-critical slip angles.
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- International Applied Mechanics, 2006, v. 42, n. 6, p. 714, doi. 10.1007/s10778-006-0139-3
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Investigation on the static and dynamic structural behaviors of a regional aircraft main landing gear by a new numerical methodology.
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- Fracture & Structural Integrity, 2018, n. 43, p. 191, doi. 10.3221/IGF-ESIS.43.15
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A field study investigating road safety effects of a front brake light.
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- IET Intelligent Transport Systems (Wiley-Blackwell), 2021, v. 15, n. 8, p. 1043, doi. 10.1049/itr2.12080
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Strain Monitoring of a Composite Drag Strut in Aircraft Landing Gear by Fiber Bragg Grating Sensors.
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- Sensors (14248220), 2019, v. 19, n. 10, p. 2239, doi. 10.3390/s19102239
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Optimization for a semi-active shock absorber using magnetorheological fluid.
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- Noise & Vibration Worldwide, 2007, v. 38, n. 10, p. 32
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Longitudinal Deck Motion Prediction and Compensation for Carrier Landing.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2013, v. 45, n. 5, p. 599
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Improved models for runway debris lofting simulations.
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- Aeronautical Journal, 2009, v. 113, n. 1148, p. 669, doi. 10.1017/S000192400000333X
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CVF ski-jump ramp profile optimisation for F-35B.
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- Aeronautical Journal, 2009, v. 113, n. 1140, p. 79, doi. 10.1017/S0001924000002803
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Monitoring of aircraft landing gear structure.
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- Aeronautical Journal, 2008, v. 112, n. 1131, p. 275, doi. 10.1017/S0001924000002220
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Investigating the Impact of Temperature Changes, Material Aging, and Service Load on the Strain of a Reinforced Concrete Construction.
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- Archives of Mining Sciences, 2014, v. 59, n. 4, p. 913, doi. 10.2478/amsc-2014-0063
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KINEMATIC ANALYSIS FOR MULTI-COPTER UAV LANDING GEAR.
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- Scientific Research & Education in the Air Force - AFASES, 2016, v. 1, p. 165, doi. 10.19062/2247-3173.2016.18.1.21
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ABOUT STRUCTURAL CONSTRUCTIV SOLUTIONS OF RETRACTABLE AIRCRAFTS' LANDING GEAR MECHANISMS.
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- Annals of 'Constantin Brancusi' University of Targu-Jiu. Engineering Series / Analele Universităţii Constantin Brâncuşi din Târgu-Jiu. Seria Inginerie, 2010, n. 4, p. 72
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Ionospheric Gradient Threat Mitigation in Future Dual Frequency GBAS.
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- International Journal of Aerospace Engineering, 2017, p. 1, doi. 10.1155/2017/4326018
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Experimental assessment of low noise landing gear component design.
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- International Journal of Aeroacoustics, 2010, v. 9, n. 6, p. 763, doi. 10.1260/1475-472X.9.6.763
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Aircraft Landing Gear Dynamics: Simulation and Control.
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- Vehicle System Dynamics, 1997, v. 28, n. 2/3, p. 119
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Dynamic Landing Response Analysis of a Flexible Tailless Delta Wing Aircraft.
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- International Journal of Aerospace Innovations, 2012, v. 4, n. 3/4, p. 103, doi. 10.1260/1757-2258.4.3-4.103
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Dynamic analysis of ground steering response of aircraft with electric taxi system.
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- Vibroengineering Procedia, 2016, v. 10, p. 358
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Towards a business enterprise strategy to support the integration of proactive aerospace maintenance technologies.
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- Insight: Non-Destructive Testing & Condition Monitoring, 2011, v. 53, n. 9, p. 502, doi. 10.1784/insi.2011.53.9.502
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Improved design of an active landing gear for a passenger aircraft using multi-objective optimization technique.
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- Structural & Multidisciplinary Optimization, 2019, v. 59, n. 5, p. 1813, doi. 10.1007/s00158-018-2135-8
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Design optimization of aircraft landing gear assembly under dynamic loading.
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- Structural & Multidisciplinary Optimization, 2018, v. 57, n. 3, p. 1357, doi. 10.1007/s00158-017-1817-y
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