Works matching DE "AIRPLANE wing design"
Results: 41
DLR natural and hybrid transonic laminar wing design incorporating new methodologies.
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- Aeronautical Journal, 2015, v. 119, n. 1221, p. 1303, doi. 10.1017/S0001924000011283
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Initial and Progressive Failure Analysis of a Composite Wing Spar Structure.
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- Journal of Mechanical Engineering (1823-5514), 2017, v. 14, n. 2, p. 169
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Aerodynamic Performances of MAV Wing Shapes.
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- Journal of Mechanical Engineering (1823-5514), 2017, v. 14, n. 2, p. 187
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Electro-Actuation System Strategy for a Morphing Flap.
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- Aerospace (MDPI Publishing), 2019, v. 6, n. 1, p. 1, doi. 10.3390/aerospace6010001
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1563. Experimental investigation of high temperature thermal-vibration characteristics for composite wing structure of hypersonic flight vehicles.
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- Journal of Vibroengineering, 2015, v. 17, n. 2, p. 917
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Characterization of the Mechanics of Compliant Wing Designs for Flapping-Wing Miniature Air Vehicles.
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- Experimental Mechanics, 2013, v. 53, n. 9, p. 1561, doi. 10.1007/s11340-013-9779-5
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Bombardier to develop materials and methods for airplane wings.
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- Advanced Materials & Processes, 2007, v. 165, n. 3, p. 19
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A Two-Level Procedure for the Global Optimum Design of Composite Modular Structures-Application to the Design of an Aircraft Wing.
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- Journal of Optimization Theory & Applications, 2012, v. 155, n. 1, p. 1, doi. 10.1007/s10957-012-0067-9
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A Two-Level Procedure for the Global Optimum Design of Composite Modular Structures-Application to the Design of an Aircraft Wing.
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- Journal of Optimization Theory & Applications, 2012, v. 155, n. 1, p. 24, doi. 10.1007/s10957-012-0070-1
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Numerical Simulation for Engine/Airframe Interaction Effects of the BWB300 on Aerodynamic Performances.
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- International Journal of Aerospace Engineering, 2019, p. 1, doi. 10.1155/2019/1072196
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Surrogate Modelling for Wing Planform Multidisciplinary Optimisation Using Model-Based Engineering.
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- International Journal of Aerospace Engineering, 2019, p. 1, doi. 10.1155/2019/4327481
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Aerodynamic Shape Design and Validation of an Advanced High-Lift Device for a Regional Aircraft with Morphing Droop Nose.
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- International Journal of Aerospace Engineering, 2019, p. 1, doi. 10.1155/2019/7982168
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Dynamic Behaviour of Mars Airplane with Folded-Wing Deployment.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 1
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New biomimetic approach to the aircraft wing structural design based on aeroelastic analysis.
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- Bulletin of the Polish Academy of Sciences: Technical Sciences, 2017, v. 65, n. 5, p. 741, doi. 10.1515/bpasts-2017-0080
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Direct measurement of the Sears function in turbulent flow.
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- Journal of Fluid Mechanics, 2018, v. 847, p. 768, doi. 10.1017/jfm.2018.351
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AIRCRAFT WINGS: PRESENT AND FUTURE.
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- Bulletin of the Transilvania University of Brasov, Series I: Engineering Sciences, 2008, v. 1, n. 50, p. 41
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IMPROVED PARTICLE SWARM OPTIMIZATION METHOD DIRECTED BY INDIRECT SURROGATE MODELING.
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- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2015, v. 8, n. 1, p. 1
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Structural design and modal behaviors analysis of a new swept baffled inflatable wing.
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- Defence Technology, 2023, v. 24, p. 382, doi. 10.1016/j.dt.2023.02.004
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Shape Reconstruction Method of Spar Wing Structure.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2014, v. 46, n. 6, p. 825
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PROBABILITY DENSITY EVOLUTION FOR TIME-VARYING RELIABILITY ASSESSMENT OF WING STRUCTURES.
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- Aviation (1648-7788), 2018, v. 22, n. 2, p. 45, doi. 10.3846/aviation.2018.6010
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Design, analysis and experimental validation of a morphing UAV wing.
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- Aeronautical Journal, 2011, v. 115, n. 1174, p. 761, doi. 10.1017/S0001924000006503
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Optimal wing twist distribution for roll control of MAVs.
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- Aeronautical Journal, 2011, v. 115, n. 1172, p. 641, doi. 10.1017/S0001924000006333
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Kinematic and experimental aerodynamic characterisation of the RotaFlap – a novel flapping wing mechanism.
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- Aeronautical Journal, 2011, v. 115, n. 1163, p. 1, doi. 10.1017/S0001924000005327
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Dynamics and control of single-line kites.
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- Aeronautical Journal, 2006, v. 110, n. 1111, p. 615
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Circular flight kite tests: converting to standard results.
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- Aeronautical Journal, 2006, v. 110, n. 1111, p. 605, doi. 10.1017/S0001924000001469
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Design of a turbulent wing for small aircraft using multidisciplinary optimisation.
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- Archives of Mechanics, 2014, v. 66, n. 3, p. 185
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MODELING OF AN AIRPLANE WING MOMENTS INDUCED BY ATMOSPHERIC TURBULENCE.
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- Proceedings of National Aviation University, 2014, v. 2, n. 59, p. 68
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CFD ANALYSIS FOR UAV OF FLYING WING.
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- Scientific Research & Education in the Air Force - AFASES, 2016, v. 1, p. 171, doi. 10.19062/2247-3173.2016.18.1.22
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Characterizing and modeling the enhancement of lift and payload capacity resulting from thrust augmentation in a propeller-assisted flapping wing air vehicle.
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- International Journal of Micro Air Vehicles, 2018, v. 10, n. 1, p. 50, doi. 10.1177/1756829317734836
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Practical Flapping Mechanisms for 20 cm-span Micro Air Vehicles.
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- International Journal of Micro Air Vehicles, 2015, v. 7, n. 2, p. 181, doi. 10.1260/1756-8293.7.2.181
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Optimal FWMAV Wing Design for a Combination of Energy-Effective Hovering and Roll Control.
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- International Journal of Micro Air Vehicles, 2015, v. 7, n. 1, p. 41, doi. 10.1260/1756-8293.7.1.41
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Numerical Study of Aerodynamic Characteristics on Blended Wing Body Aircraft with Small Canard.
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- Pertanika Journal of Science & Technology, 2017, v. 25, n. S, p. 9
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ASLO 2023 Award Winners—Part I.
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- Limnology & Oceanography Bulletin, 2023, v. 32, n. 3, p. 107, doi. 10.1002/lob.10594
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Large-scale stabilization control of input-constrained quadrotor.
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- International Journal of Advanced Robotic Systems, 2016, v. 13, n. 5, p. 1, doi. 10.1177/1729881416670109
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Extended discrete-time transfer matrix approach to modeling and decentralized control of lattice-based structures.
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- Structural Control & Health Monitoring, 2016, v. 23, n. 10, p. 1256, doi. 10.1002/stc.1837
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Aeroelastic Control of a Wing with Active Skins Using Piezoelectric Patches.
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- Mechanics of Advanced Materials & Structures, 2007, v. 14, n. 1, p. 23, doi. 10.1080/15376490600864505
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Wing Aerodynamic Optimization by Using Genetic Algoritm and Ansys.
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- Acta Physica Polonica: A, 2017, v. 132, n. 3, p. 981, doi. 10.12693/APhysPolA.132.981
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Constraint aggregation for large number of constraints in wing surrogate-based optimization.
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- Structural & Multidisciplinary Optimization, 2019, v. 59, n. 2, p. 421, doi. 10.1007/s00158-018-2074-4
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Concurrent wing and high-lift system aerostructural optimization.
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- Structural & Multidisciplinary Optimization, 2018, v. 57, n. 3, p. 947, doi. 10.1007/s00158-017-1787-0
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Aircraft morphing wing design by using partial topology optimization.
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- Structural & Multidisciplinary Optimization, 2013, v. 48, n. 6, p. 1109, doi. 10.1007/s00158-013-0944-3
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Winglet geometry effects on tip leakage loss over the plane tip in a turbine cascade.
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- Journal of Mechanical Science & Technology, 2018, v. 32, n. 4, p. 1633, doi. 10.1007/s12206-018-0318-2
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