Works matching DE "MATHEMATICAL models of aerodynamics"
Results: 68
Immersed boundary method as applied to the simulation of external aerodynamics problems with various boundary conditions.
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- Doklady Mathematics, 2015, v. 91, n. 2, p. 178, doi. 10.1134/S1064562415020192
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Flap/Lag Stall Flutter Control of Large-Scale Wind Turbine Blade Based on Robust H<sub>2</sub> Controller.
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- Shock & Vibration, 2016, p. 1, doi. 10.1155/2016/8378161
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Calculus model in quasi - velocity frame for small launcher, technical solution.
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- Mathematics in Engineering, Science & Aerospace (MESA), 2015, v. 6, n. 1, p. 73
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Space-time techniques for computational aerodynamics modeling of flapping wings of an actual locust.
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- Computational Mechanics, 2012, v. 50, n. 6, p. 743, doi. 10.1007/s00466-012-0759-x
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Physicomathematical Simulation Analysis for Small Bullets.
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- Journal of Engineering Science & Technology Review, 2008, v. 1, n. 1, p. 70
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La Secuencia de Fibonacci y el Número de Oro en Ingeniería Eléctrica y Análisis Numérico.
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- Formación Universitaria, 2013, v. 6, n. 2, p. 23, doi. 10.4067/S0718-50062013000200004
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Dust deposition and ambient PM<sub>10</sub> concentration in northwest China: spatial and temporal variability.
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- Atmospheric Chemistry & Physics, 2017, v. 17, n. 3, p. 1699, doi. 10.5194/acp-17-1699-2017
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Hydro- and aerodynamic analysis for the design of a sailing yacht.
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- Journal of Marine Science & Technology, 2010, v. 15, n. 3, p. 230, doi. 10.1007/s00773-010-0088-8
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DAE-index monitoring for semi-discretized viscous Cosserat rod models.
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- PAMM: Proceedings in Applied Mathematics & Mechanics, 2013, v. 13, n. 1, p. 501, doi. 10.1002/pamm.201310243
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MODELADO Y CONTROL DE UN PROTOTIPO DE AERONAVE NO TRIPULADO DE ALA FIJA.
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- Revista Politécnica, 2014, v. 10, n. 18, p. 93
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Preliminary Design Estimation of the V/STOL Airplane Performance.
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- International Journal of Micro Air Vehicles, 2015, v. 7, n. 4, p. 55, doi. 10.1260/1756-8293.7.4.449
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A Review of Biomimetic Air Vehicle Research: 1984-2014.
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- International Journal of Micro Air Vehicles, 2015, v. 7, n. 3, p. 375, doi. 10.1260/1756-8293.7.3.375
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A CFD Study on Leading Edge Wing Surface Modification of a Low Aspect Ratio Flying wing to Improve Lift Performance.
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- International Journal of Micro Air Vehicles, 2015, v. 7, n. 3, p. 361, doi. 10.1260/1756-8293.7.3.361
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A Numerical Model to Study the Nonlinear and Unsteady Aerodynamics of Bioinspired Morphing-Wing Concepts.
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- International Journal of Micro Air Vehicles, 2015, v. 7, n. 3, p. 327, doi. 10.1260/1756-8293.7.3.327
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On the Unsteady Behavior of the Flow Around NACA 0012 Airfoil with Steady External Conditions at Re=1000.
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- International Journal of Micro Air Vehicles, 2015, v. 7, n. 3, p. 301, doi. 10.1260/1756-8293.7.3.301
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A Monte Carlo Analysis of Sensor Fusion Algorithm for the Estimation of Aerodynamic Angles in a Mini Aerial Vehicle.
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- International Journal of Micro Air Vehicles, 2011, v. 3, n. 1, p. 35, doi. 10.1260/1756-8293.3.1.35
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About restrictions on maximum velocity in inverse boundary-value problems of aerohydrodynamics.
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- Doklady Physics, 2010, v. 55, n. 2, p. 89, doi. 10.1134/S1028335810020114
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Experimental Research on an Active Sting Damper in a Low Speed Acoustic Wind Tunnel.
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- Shock & Vibration, 2014, p. 1, doi. 10.1155/2014/524351
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An Improved Low-Reynolds-Number k - ϵ Model for Aerodynamic Flows.
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- International Journal of Nonlinear Sciences & Numerical Simulation, 2016, v. 17, n. 2, p. 99, doi. 10.1515/ijnsns-2015-0175
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Numerical computation of the flow around two square cylinders arranged side-by-side.
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- Applied Mathematics & Mechanics, 2000, v. 21, n. 2, p. 147, doi. 10.1007/BF02458515
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Lagrange's Equations for Rocket-Type Variable Mass Systems.
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- International Review of Aerospace Engineering, 2012, v. 5, n. 5, p. 256, doi. 10.15866/irease.v5i5.15613
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Numerical Analysis of Anti-Icing and De-Icing Thermal Systems.
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- International Review of Aerospace Engineering, 2012, v. 5, n. 4, p. 117
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Development and characterization of a single particle laser ablation mass spectrometer (SPLAM) for organic aerosol studies.
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- Atmospheric Measurement Techniques, 2012, v. 5, n. 1, p. 225, doi. 10.5194/amt-5-225-2012
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Hit and flip.
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- Nature Physics, 2015, v. 11, n. 6, p. 443, doi. 10.1038/nphys3360
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Comprehensive evaluation and assessment of trailing edge noise prediction based on dedicated measurements.
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- Noise Control Engineering Journal, 2011, v. 59, n. 1, p. 54, doi. 10.3397/1.3531794
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Aerodynamic web forming: process simulation and material properties.
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- Journal of Mathematics in Industry, 2016, v. 6, n. 1, p. 1, doi. 10.1186/s13362-016-0034-4
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USING OF THE FINITE ELEMENT METHOD IN EXTERIOR BALLISTICS.
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- Buletin Stiintific, 2009, v. 14, n. 2, p. 111
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Comparison of Three Coaxial Aerodynamic Prediction Methods Including Validation with Model Test Data.
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- Journal of the American Helicopter Society, 2014, v. 59, n. 3, p. 032006-1, doi. 10.4050/JAHS.59.032006
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Numerical characterization of three-dimensional bluff body shear layer behaviour.
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- Journal of Fluid Mechanics, 2016, v. 799, p. 1, doi. 10.1017/jfm.2016.344
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Constrained pseudo-transient continuation.
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- International Journal for Numerical Methods in Engineering, 2015, v. 102, n. 11, p. 1683, doi. 10.1002/nme.4858
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Aerodynamic Optimization of Airfoils Using Adaptive Parameterization and Genetic Algorithm.
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- Journal of Optimization Theory & Applications, 2014, v. 162, n. 1, p. 257, doi. 10.1007/s10957-013-0442-1
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Air stream velocity modelling in multichannel spiral cyclone separator.
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- Journal of Environmental Engineering & Landscape Management, 2014, v. 22, n. 3, p. 183, doi. 10.3846/16486897.2014.931283
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Active flutter suppression control law design method based on balanced proper orthogonal decomposition reduced order model.
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- Nonlinear Dynamics, 2012, v. 70, n. 1, p. 1, doi. 10.1007/s11071-012-0392-4
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An efficient method for nonlinear aeroelasticy of slender wings.
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- Nonlinear Dynamics, 2012, v. 67, n. 1, p. 659, doi. 10.1007/s11071-011-0018-2
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Stochastic modeling of lift and drag dynamics under turbulent wind inflow conditions.
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- Wind Energy, 2015, v. 18, n. 2, p. 317, doi. 10.1002/we.1699
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Effects of nonuniform incident velocity on a dynamic wind turbine airfoil.
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- Wind Energy, 2015, v. 18, n. 2, p. 237, doi. 10.1002/we.1694
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Inverse design of horizontal axis wind turbine blades using a vortex line method.
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- Wind Energy, 2015, v. 18, n. 2, p. 253, doi. 10.1002/we.1695
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Wind turbine rotor imbalance detection using nacelle and blade measurements.
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- Wind Energy, 2015, v. 18, n. 2, p. 267, doi. 10.1002/we.1696
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Analysis of New Aerodynamic Design of the Nose Cone Section Using CFD and SPH.
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- INCAS Bulletin, 2015, v. 7, n. 2, p. 43, doi. 10.13111/2066-8201.2015.7.2.4
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Wing Geometry and Kinematic Parameters Optimization of Flapping Wing Hovering Flight.
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- Applied Sciences (2076-3417), 2016, v. 6, n. 12, p. 390, doi. 10.3390/app6120390
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A Cost-Effective Tracking Algorithm for Hypersonic Glide Vehicle Maneuver Based on Modified Aerodynamic Model.
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- Applied Sciences (2076-3417), 2016, v. 6, n. 10, p. 312, doi. 10.3390/app6100312
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Experimental and numerical analysis of aerodynamic effects of repair patches on damaged airfoils.
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- Journal of Mechanical Science & Technology, 2017, v. 31, n. 2, p. 651, doi. 10.1007/s12206-016-1220-4
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Higher-order reverse automatic differentiation with emphasis on the third-order.
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- Mathematical Programming, 2016, v. 155, n. 1/2, p. 81, doi. 10.1007/s10107-014-0827-4
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Transformable descent vehicles.
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- Solar System Research, 2016, v. 50, n. 7, p. 489, doi. 10.1134/S0038094616070200
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Preliminary design of pseudo satellites: Basic methods and feasibility criteria.
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- Solar System Research, 2016, v. 50, n. 7, p. 523, doi. 10.1134/S0038094616070091
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Araç Dinamiği Modellenmesi, Simülasyonu ve Görselleştirilmesi.
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- Journal of Defense Sciences / Savunma Bilmleri Dergisi, 2012, v. 11, n. 1, p. 133
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PLANIFICACIÓN DE TRAYECTORIAS PARA UN ROBOT TIPO CON RESTRICCIONES DINÁMICAS.
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- Ciencia e Ingenieria Neogranadina, 2008, v. 18, n. 1, p. 75
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APROXIMACIÓN AL CONTROL DE LA FASE DE VUELO DE UN DIRIGIBLE.
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- Ciencia e Ingenieria Neogranadina, 2008, v. 18, n. 1, p. 51, doi. 10.18359/rcin.1068
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Effects of blade configuration parameters on helicopter rotor structural dynamics and whirl tower loads.
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- Aeronautical Journal, 2016, v. 120, n. 1224, p. 271, doi. 10.1017/aer.2015.11
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Estimation of lateral-directional aerodynamic derivatives from flight data using conventional and neural based methods.
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- Aeronautical Journal, 2014, v. 118, n. 1210, p. 1453, doi. 10.1017/S0001924000010149
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