Works matching DE "HELICOPTER rotor aerodynamics"
Results: 39
Fast Axial Positioning with Linear⁃Velocity Control for Linear⁃Rotary Switched Reluctance Motor.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2024, v. 41, n. 3, p. 300, doi. 10.16356/j.1005⁃1120.2024.03.004
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Rotor Displacement Control of Bearingless Switched Reluctance Motor with Single⁃Winding Stator.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2024, v. 41, n. 3, p. 289, doi. 10.16356/j.1005⁃1120.2024.03.003
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Rotor Vibratory Load Reduction by Piecewise Linear Blade Twist.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2024, v. 41, n. 3, p. 278, doi. 10.16356/j.1005‑1120.2024.03.002
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New Progress in Helicopter Rotor Wake Research.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2019, v. 36, n. 1, p. 36, doi. 10.16356/j.1005-1120.2019.01.004
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Numerical Simulation of Aerodynamic Characteristics of Helicopter Rotor with Tip Slots.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2018, v. 35, n. 6, p. 942, doi. 10.16356/j.1005-1120.2018.06.942
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ATTENUATION AVERAGE SIGNAL POWER HELICOPTER ANTENNA SYSTEM.
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- Electronics & Control Systems, 2015, v. 44, n. 2, p. 11
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Closed-Form Aerodynamic Derivatives of Multicopter Propellers in General Motion.
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- International Journal of Simulation: Systems, Science & Technology, 2017, v. 18, n. 3, p. 2.1, doi. 10.5013/IJSSST.a.18.03.02
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Dynamic Simulation of an Unmanned Hybrid Flying Robot.
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- International Journal of Micro Air Vehicles, 2015, v. 7, n. 3, p. 257, doi. 10.1260/1756-8293.7.3.257
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Indoor/Outdoor Scan-Matching Based Mapping Technique with a Helicopter MAV in GPS-Denied Environment.
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- International Journal of Micro Air Vehicles, 2015, v. 7, n. 1, p. 55, doi. 10.1260/1756-8293.7.1.55
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Reviewing and Investigating the Use of Co-Axial Rotor Systems in Small UAVs.
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- International Journal of Micro Air Vehicles, 2010, v. 2, n. 1, p. 1, doi. 10.1260/1756-8293.2.1.1
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Time-Accurate Aeroelastic Computations of a Full Helicopter Model using the Navier-Stokes Equations.
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- International Journal of Aerospace Innovations, 2013, v. 5, n. 3/4, p. 73, doi. 10.1260/1757-2258.5.3-4.73
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Development of 10DOF Nonlinear Model of an Autonomous Helicopter with Control Rotor System.
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- International Review of Aerospace Engineering, 2009, v. 2, n. 4, p. 199
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Multilayer hierarchical control for robotic coax-helicopter based on the H∞ robustness and mixing control scheme.
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- Advances in Mechanical Engineering (Sage Publications Inc.), 2017, v. 9, n. 10, p. 1, doi. 10.1177/1687814017720088
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Unsteady Load Calculation for Rotor Based on VVPM/CA Coupling.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2014, v. 46, n. 3, p. 443
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Cracking of Erosion Strip of Main Rotor Blade of a Military Helicopter.
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- Journal of Failure Analysis & Prevention, 2019, v. 19, n. 1, p. 36, doi. 10.1007/s11668-019-00594-1
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Failure Analysis of an Air Turbine Starter.
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- Journal of Failure Analysis & Prevention, 2010, v. 10, n. 4, p. 259, doi. 10.1007/s11668-010-9350-y
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Technical Note Estimate of Rotor Controls and Blade Flapping Caused by an Orthogonal Vortex Disturbance.
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- Journal of the American Helicopter Society, 2018, v. 63, n. 2, p. 1, doi. 10.4050/JAHS.63.025001
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A Dynamic-Inflow-Based Induced Power Model for General and Optimal Rotor Performance.
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- Journal of the American Helicopter Society, 2018, v. 63, n. 2, p. 1, doi. 10.4050/JAHS.63.022008
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Comparison of CAMRAD II and RCAS Predictions of Tiltrotor Aeroelastic Stability.
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- Journal of the American Helicopter Society, 2018, v. 63, n. 2, p. 1, doi. 10.4050/JAHS.63.022001
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- Article
Helicopter Main Rotor Hub Load Alleviation Using a Variable Incidence Horizontal Stabilizer.
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- Journal of the American Helicopter Society, 2018, v. 63, n. 1, p. 1, doi. 10.4050/JAHS.63.012005
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Computational Aeroelasticity of Rotating Wings with Deformable Airfoils.
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- Journal of the American Helicopter Society, 2017, v. 62, n. 3, p. 1, doi. 10.4050/JAHS.62.032006
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Aerodynamic Performance of a Hovering Microrotor in Confined Environment.
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- Journal of the American Helicopter Society, 2017, v. 62, n. 2, p. 022008-1, doi. 10.4050/JAHS.62.022008
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Extracting Blade–Vortex Interactions Using Continuous Wavelet Transforms.
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- Journal of the American Helicopter Society, 2017, v. 62, n. 2, p. 022001-1, doi. 10.4050/JAHS.62.022001
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Hover Performance Measurements Toward Understanding Aerodynamic Interference in Coaxial, Tandem, and Tilt Rotors.
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- Journal of the American Helicopter Society, 2015, v. 60, n. 3, p. 1, doi. 10.4050/JAHS.60.032005
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Modular Multisolver Approach for Efficient High-Fidelity Simulation of the HART II Rotor.
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- Journal of the American Helicopter Society, 2015, v. 60, n. 3, p. 1, doi. 10.4050/JAHS.60.032001
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Extendable Chord Rotors for Helicopter Envelope Expansion and Performance Improvement.
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- Journal of the American Helicopter Society, 2014, v. 59, p. 1, doi. 10.4050/JAHS.59.012007
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Background-Oriented Schlieren Imaging for Full-Scale and In-Flight Testing.
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- Journal of the American Helicopter Society, 2014, v. 59, p. 1, doi. 10.4050/JAHS.59.012002
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Experimental Investigation of Unsteady Transition on a Pitching Rotor Blade Airfoil.
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- Journal of the American Helicopter Society, 2014, v. 59, p. 1, doi. 10.4050/JAHS.59.012001
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Application of Low- and High-Fidelity Simulation Tools to Helicopter Rotor Blade Optimization.
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- Journal of the American Helicopter Society, 2013, v. 58, p. 1, doi. 10.4050/JAHS.58.042003
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Mathematical modelling of the rotor of a helicopter with ejection devices.
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- Russian Journal of Numerical Analysis & Mathematical Modelling, 1999, v. 14, n. 3, p. 237, doi. 10.1515/rnam.1999.14.3.237
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- Article
KUYRUK ROTORSUZ TEST HELİKOPTERİ VE TEST DÜZENEĞİ TASARIMI.
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- Teknoloji, 2004, v. 7, n. 4, p. 659
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Nonlinear aeroelastic stability analysis of hingeless helicopter rotor blades using FRF coupling and condition number.
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- Nonlinear Dynamics, 2015, v. 82, n. 1/2, p. 289, doi. 10.1007/s11071-015-2157-3
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Attitude Tracking Control of A Quad-Rotor with Partial Loss of Rotation Effectiveness.
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- Asian Journal of Control, 2017, v. 19, n. 5, p. 1812, doi. 10.1002/asjc.1495
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Control laws for an active tunable vibration absorber designed for rotor blade damping augmentation.
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- Aeronautical Journal, 2004, v. 108, n. 1079, p. 35, doi. 10.1017/S0001924000004978
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Unusual Aggregation-Induced Emission of a Coumarin Derivative as a Result of the Restriction of an Intramolecular Twisting Motion.
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- Angewandte Chemie, 2015, v. 127, n. 48, p. 14700, doi. 10.1002/ange.201506782
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Lagrangian formulation for the rapid estimation of helicopter rotor blade vibration characteristics.
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- Aeronautical Journal, 2014, v. 118, n. 1206, p. 861, doi. 10.1017/S000192400000960X
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Operational performance of inlet barrier filters for rotorcraft.
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- Aeronautical Journal, 2012, v. 116, n. 1182, p. 847, doi. 10.1017/S0001924000007314
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Non-linear control algorithm for the four rotors UAV attitude tracking problem.
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- Aeronautical Journal, 2011, v. 115, n. 1165, p. 175, doi. 10.1017/S0001924000005571
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Flow visualisation of the helicopter brown-out phenomenon.
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- Aeronautical Journal, 2009, v. 113, n. 1145, p. 467, doi. 10.1017/S0001924000003134
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