Works matching DE "WIND tunnel testing"
Results: 1321
Numerical and experimental validation of a morphed wing geometry using Price-Païdoussis wind-tunnel testing.
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- Aeronautical Journal, 2016, v. 120, n. 1227, p. 757, doi. 10.1017/aer.2016.30
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Estimating aerofoil lift from flow angle.
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- Aeronautical Journal, 2015, v. 119, n. 1219, p. 1167, doi. 10.1017/S0001924000011180
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Aerodynamic modelling of fin stabilised underslung loads.
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- Aeronautical Journal, 2015, v. 119, n. 1219, p. 1073, doi. 10.1017/S0001924000011143
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The influence of simulated missile warhead fragment damage on the aerodynamic characteristics of two-dimensional wings.
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- Aeronautical Journal, 2013, v. 117, n. 1194, p. 823, doi. 10.1017/S0001924000008472
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Aerodynamics of an aerofoil in transonic ground effect: Methods for blowdown wind-tunnel scale testing.
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- Aeronautical Journal, 2012, v. 116, n. 1180, p. 599, doi. 10.1017/S0001924000007090
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Application of aerodynamic model structure determination to UAV data.
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- Aeronautical Journal, 2011, v. 115, n. 1170, p. 481, doi. 10.1017/S0001924000006126
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Flow field and performance analysis of an integrated diverterless supersonic inlet.
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- Aeronautical Journal, 2011, v. 115, n. 1170, p. 471, doi. 10.1017/S0001924000006114
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The influence of Reynolds and Mach numbers on two-dimensional wind-tunnel testing: An experience.
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- Aeronautical Journal, 2011, v. 115, n. 1166, p. 249, doi. 10.1017/S0001924000005704
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Helicopter icing.
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- Aeronautical Journal, 2010, v. 114, n. 1152, p. 83, doi. 10.1017/S0001924000003559
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Flutter/LCO suppression for high-aspect ratio wings.
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- Aeronautical Journal, 2009, v. 113, n. 1144, p. 409, doi. 10.1017/S0001924000003079
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Wind tunnel testing of powered lift, ale-wing STOL model.
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- Aeronautical Journal, 2009, v. 113, n. 1140, p. 129, doi. 10.1017/S0001924000002840
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Highlights of the Lockheed Martin F-35 STOVL jet effects programme.
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- Aeronautical Journal, 2009, v. 113, n. 1140, p. 119, doi. 10.1017/S0001924000002864
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A circulation control actuator for flapless flight control.
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- Aeronautical Journal, 2008, v. 112, n. 1134, p. 483, doi. 10.1017/S0001924000002451
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An Original Aerodynamic Ducting System to Improve Energy Efficiency in the Automotive Industry.
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- Inventions (2411-5134), 2023, v. 8, n. 1, p. 13, doi. 10.3390/inventions8010013
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COMPUTATIONAL AND EXPERIMENTAL ANALYSIS OF A DIFFUSER THAT CONSTITUTES A CONCEPTUAL AND UNPRECEDENTED DAWT FOR URBAN APPLICATIONS.
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- Revista Foco (Interdisciplinary Studies Journal), 2024, v. 17, n. 1, p. 1, doi. 10.54751/revistafoco.v17n1-125
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篱墙对街谷中机动车排放CO扩散的影响研究.
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- Environmental Science & Technology (10036504), 2021, v. 44, n. 11, p. 48, doi. 10.19672/j.cnki.1003-6504.1513.21.338
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Unsteady dynamics and organized structures from DNS over an idealized building canopy.
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- International Journal of Climatology, 2007, v. 27, n. 14, p. 1943, doi. 10.1002/joc.1549
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A Wood-Strand Material for Wind Erosion Control: Effects on Total Sediment Loss, PM<sub>10</sub> Vertical Flux, and PM<sub>10</sub> Loss.
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- Journal of Environmental Quality, 2009, v. 38, n. 1, p. 139, doi. 10.2134/jeq2008.0115
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AWWA Water Science Author Spotlight.
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- Journal: American Water Works Association, 2021, v. 113, n. 3, p. 14, doi. 10.1002/awwa.1687
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Preface to the Special Issue of JSSM dedicated to the Life of Professor Paul Lagacé.
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- Journal of Sandwich Structures & Materials, 2023, v. 25, n. 1, p. 3, doi. 10.1177/10996362221148249
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- Article
Flight-to-Wind-Tunnel Correlation Study using JAXA's Flying Test Bed "Hisho".
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- Transactions of the Japan Society of Aeronautical & Space Science, 2023, v. 66, n. 2, p. 17, doi. 10.2322/tjsass.66.17
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Numerical Analysis on Axial Force Characteristics of Reusable Launch Vehicle at 150-180° Angles of Attack.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2023, v. 66, n. 4, p. 118, doi. 10.2322/tjsass.66.118
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Capture Area Ratio and Drag Difference between Wind Tunnel and Flight Tests.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2022, v. 65, n. 3, p. 134, doi. 10.2322/tjsass.65.134
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Numerical/Experimental Hybrid Study on Base Pressure and Cavity Pressure Corrections for Transonic Wind Tunnel Tests.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2022, v. 65, n. 3, p. 116, doi. 10.2322/tjsass.65.116
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Added Masses of an Elliptical Cylinder with Unsteady Motion or in Unsteady Flow.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2021, v. 64, n. 6, p. 358, doi. 10.2322/tjsass.64.358
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Feasibility Study on Real-time Observation of Flow Velocity Field using Sparse Processing Particle Image Velocimetry.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2021, v. 64, n. 4, p. 242, doi. 10.2322/tjsass.64.242
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Supersonic Ejector-Driving System under Low Pressure: A Performance Evaluation.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2021, v. 64, n. 3, p. 156, doi. 10.2322/tjsass.64.156
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Measurement of Unsteady Aerodynamic Characteristics of a Heaving Wing in a Low Reynolds Number Flow.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2021, v. 64, n. 3, p. 147, doi. 10.2322/tjsass.64.147
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Effects of Propeller Position and Rotation Direction on the Ishii Wing at a Low Reynolds Number.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2021, v. 64, n. 1, p. 22, doi. 10.2322/tjsass.64.22
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Estimating Aerodynamic Coefficients from Uncertain Data of D-SEND Aircraft with Gaussian Process Regression.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2020, v. 63, n. 6, p. 257, doi. 10.2322/tjsass.63.257
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Abstracts of the Papers Published in Journal of the Japan Society for Aeronautical and Space Sciences.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2020, v. 63, n. 2, p. 66, doi. 10.2322/tjsass.63.66
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Experimental Study about the Deformation and Aerodynamic Characteristics of the Passive Morphing Airfoil.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2020, v. 63, n. 1, p. 18, doi. 10.2322/tjsass.63.18
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Disappearance of Vortex Lift in Low-Aspect-Ratio Wings at Very-low Reynolds Numbers.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2019, v. 62, n. 6, p. 310, doi. 10.2322/tjsass.62.310
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In-Flight Measurement of Wing Deformation.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2019, v. 62, n. 2, p. 108, doi. 10.2322/tjsass.62.108
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Correction of Wind Tunnel Test Data for Additional Roughness Drag.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2018, v. 61, n. 1, p. 21, doi. 10.2322/tjsass.61.21
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Mach Number Effect on Supersonic Drag Reduction using Repetitive Laser Energy Depositions over a Blunt Body.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2017, v. 60, n. 5, p. 303, doi. 10.2322/tjsass.60.303
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An experimental investigation and flow field analysis on cycling clothing fabrics with grooved surface.
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- Journal of Industrial Textiles, 2022, v. 52, p. 1, doi. 10.1177/15280837221142034
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An experimental investigation and flow field analysis on cycling clothing fabrics with grooved surface.
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- Journal of Industrial Textiles, 2022, v. 52, p. 1, doi. 10.1177/15280837221142034
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Flutter performance of shape memory alloy-embedded 3D woven flexible composite plate under subsonic flow.
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- Journal of Industrial Textiles, 2022, v. 51, p. 4290S, doi. 10.1177/15280837221077043
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Development of scheme to evaluate the performance of parachute canopy fabrics under tensile impact.
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- Journal of Industrial Textiles, 2022, v. 51, p. 2283S, doi. 10.1177/15280837221080103
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Aerodynamic performance of the supersonic parachute with material permeability.
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- Journal of Industrial Textiles, 2021, v. 50, n. 6, p. 812, doi. 10.1177/1528083719844605
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A Comparison of the Surface Pressure Distribution of Circular Cables and Helical Fillet Cables under Wind Attack: A Wind Tunnel Test Study.
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- Engineering, Technology & Applied Science Research, 2024, v. 14, n. 4, p. 15393, doi. 10.48084/etasr.7602
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大跨度柔性光伏支架阵列极值风荷载与干扰效应.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2024, v. 56, n. 6, p. 1161, doi. 10.16356/j.1005-2615.2024.06.020
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小型巡飞弹螺旋桨气动优化设计.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2024, v. 56, n. 4, p. 698, doi. 10.16356/j.1005-2615.2024.04.012
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基于电加热膜防冰设计方案的分流环表面换热特性 试验研究.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2023, v. 55, n. 2, p. 249, doi. 10.16356/j.1005‑2615.2023.02.010
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冰风洞过冷大水滴云雾水滴质量分布模拟 .
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2023, v. 55, n. 1, p. 146, doi. 10.16356/j.1005‑2615.2023.01.018
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平尾防冰表面溢流冰生成规律试验研究.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2022, v. 54, n. 6, p. 1074, doi. 10.16356/j.1005‑2615.2022.06.009
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机动弹头舵轴热环境分析.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2022, v. 54, n. 4, p. 583, doi. 10.16356/j.1005-2615.2022.04.005
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低速风洞试验模型振动主动控制技术.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2021, v. 53, n. 4, p. 591, doi. 10.16356/j.1005-2615.2021.04.013
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无人旋翼机旋翼气动分析与试验研究.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2021, v. 53, n. 2, p. 253, doi. 10.16356/j.1005⁃2615.2021.02.012
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