Basic and Applied Science OA Books Collection
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Browsing Basic and Applied Science OA Books Collection by Subject "Aerodynamics"
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Item a Computer-Assisted Wind Load Evaluation System For The Design of Cladding of Buildings(IntechOpen, 2023) Yasushi UematsuA Computer-Assisted Wind Load Evaluation System for the Design of Cladding of Buildings: a Case Study of Spatial StructuresItem A Method of Evaluating the Presence of Fan-Blade-Rotation Induced Unsteadiness in Wind Tunnel Experiments(IntechOpen, 2023) Josue Njock LibiiA Method of Evaluating the Presence of Fan-Blade-Rotation Induced Unsteadiness in Wind Tunnel ExperimentsItem A Methodology Based on Experimental Investigation of a DBD-Plasma Actuated Cylinder Wake for Flow Control(IntechOpen, 2023) Kelly CohenA Methodology Based on Experimental Investigation of a DBD-Plasma Actuated Cylinder Wake for Flow ControlItem Active and Passive Control of Flow Past a Cavity(IntechOpen, 2023) Seiichiro IzawaActive and Passive Control of Flow Past a CavityItem Aerodynamic and Aeroacoustic Study of a High Rotational Speed Centrifugal Fan(IntechOpen, 2023) Sofiane KhelladiAerodynamic and Aeroacoustic Study of a High Rotational Speed Centrifugal FanItem Aerodynamic Design of Sports Garments(IntechOpen, 2023) Harun ChowdhuryAerodynamic Design of Sports GarmentsItem Aerodynamic Parameters on a Multisided Cylinder for Fatigue Design(IntechOpen, 2023) Byungik ChangAerodynamic Parameters on a Multisided Cylinder for Fatigue DesignItem Aerodynamic Performance of the Flapping Wing(IntechOpen, 2023) Abbas EbrahimiAerodynamic Performance of the Flapping WingItem Afterburning Installation Integration into a Cogeneration Power Plant with Gas Turbine by Numerical and Experimental Analysis(IntechOpen, 2023) Ene BarbuAfterburning Installation Integration into a Cogeneration Power Plant with Gas Turbine by Numerical and Experimental AnalysisItem Air Speed Measurement Standards Using Wind Tunnels(IntechOpen, 2023) Sejong ChunAir Speed Measurement Standards Using Wind TunnelsItem An Approximate Riemann Solver for Euler Equations(IntechOpen, 2023) Oscar FalcinelliAn Approximate Riemann Solver for Euler EquationsItem Application of Statistical Methods for Gas Turbine Plant Operation Monitoring(IntechOpen, 2023) Li PanApplication of Statistical Methods for Gas Turbine Plant Operation MonitoringItem Biofuel and Gas Turbine Engines(IntechOpen, 2023) Marco Antonio Rosa do NascimentoBiofuel and Gas Turbine EnginesItem BLISK Fabrication by Linear Friction Welding(IntechOpen, 2023) Antonio M. Mateo GarciaBLISK Fabrication by Linear Friction WeldingItem Bluff Body Aerodynamics and Wake Control(IntechOpen, 2023) Efstathios KonstantinidisBluff Body Aerodynamics and Wake ControlItem Characterization of a Spray in the Combustion Chamber of a Low Emission Gas Turbine(IntechOpen, 2023) Georges DescombesCharacterization of a Spray in the Combustion Chamber of a Low Emission Gas TurbineItem Comparison between Semiempirical and Computational Techniques in the Prediction of Aerodynamic Performance of the Rotor of a Quadcopter(IntechOpen, 2023) Andres Mauricio PerezUnmanned aerial vehicle (UAV) is a growing technology used in different industries, and the main platform used for the UAVs is the quadcopter. The rotor of a quadcopter typically operates at low to moderate Reynolds number, so that the aerodynamics and an early prediction of the performance of the propellers are important in the design of the quadcopter. In the present chapter, the performance of a commercial propeller used in quadcopters is analyzed with three different techniques: momentum theory, blade element theory, and computational fluid dynamics. By applying the momentum and blade element theory, it was possible to estimate the thrust generated for a propeller in hover. A computational model based on computational fluid dynamics (CFD) was implemented and used to simulate a propeller in hover; the model predicts the wake and the thrust of the propeller as well. The results of the theory and computational approximations were compared with experimental measurements of flying tests.Item Comparison of Aerodynamic Effects Promoted by Mechanical and Fluidic Miniflaps on an Airfoil NACA 4412(IntechOpen, 2023) M. CasperComparison of Aerodynamic Effects Promoted by Mechanical and Fluidic Miniflaps on an Airfoil NACA 4412Item Components of a Wind Tunnel Balance(IntechOpen, 2023) Miguel GonzalezComponents of a Wind Tunnel Balance: Design and CalibrationItem Computational Aeroelasticity of Flying Robots with Flexible Wings(IntechOpen, 2023) Sergio PreidikmanA computational co?simulation framework for flying robots with flexible wings is presented. The authors combine a nonlinear aerodynamic model based on an extended version of the unsteady vortex?lattice method with a nonlinear structural model based on a segregated formulation of Lagrange's equations obtained with the Floating Frame of Reference formalism. The structural model construction allows for hybrid combinations of different models typically used with multibody systems such as models based on rigid?body dynamics, assumed?modes techniques, and finite?element methods. The aerodynamic model includes a simulation of leading?edge separation for large angles of attack. The governing differential?algebraic equations are solved simultaneously and interactively to obtain the structural response and the flow in the time domain. The integration is based on the fourth?order predictor?corrector method of Hamming with a procedure to stabilize the iteration. The findings are found to capture known nonlinear behavior of flapping-wing systems. The developed framework should be relevant for conducting aeroelastic studies on a wide variety of air vehicle systems.