Search results for "Transonic"

showing 4 items of 4 documents

Shock control bump design optimization on natural laminar aerofoil

2011

The chapter investigates Shock Control Bumps (SCB) on a Natural Laminar Flow (NLF) aerofoil; RAE 5243 for Active Flow Control (AFC). A SCB approach is used to decelerate supersonic flow on the suction/pressure sides of transonic aerofoil that leads delaying shock occurrence or weakening of shock strength. Such an AFC technique reduces significantly the total drag at transonic speeds. This chapter considers the SCB shape design optimisation at two boundary layer transition positions (0 and 45%) using an Euler software coupled with viscous boundary layer effects and robust Evolutionary Algorithms (EAs). The optimisation method is based on a canonical Evolution Strategy (ES) algorithm and inco…

AirfoilHybrid OptimisationEngineeringUAVAvions -- AlesDrag Reduction:Matemàtiques i estadística::Anàlisi numèrica [Àrees temàtiques de la UPC]Aerofoils--Mathematical modelsTransition pointWave dragAerospace engineeringAerodinàmica -- Mètodes numèricsSuction Sidebusiness.industry:Matemàtiques i estadística::Anàlisi numèrica::Mètodes numèrics [Àrees temàtiques de la UPC]Laminar flow010303 Optimisation090100 AEROSPACE ENGINEERINGMechanicsBoundary Layer TransitionACTIVE FLOW CONTROL:Aeronàutica i espai::Aerodinàmica [Àrees temàtiques de la UPC]Superfícies de sustentacióLift (force)Boundary layerWave DragDragUASbusinessBaseline DesignTransonic090104 Aircraft Performance and Flight Control Systems
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Nonlocality and fluctuations near the optical analog of a sonic horizon

2013

We consider the behavior of fluctuations near the sonic horizon and the role of the nonlocality of interaction (nonlinearity) on their regularization. The nonlocality dominates if its characteristic length scale is larger than the regularization length. The influence of nonlocality may be important in the current experiments on the transonic flow in Kerr nonlinear media. Experimental conditions, under which the observation of straddled fluctuations can be observed, are discussed.

PhysicsNonlinear systemQuantum nonlocalityCharacteristic lengthQuantum mechanicsRegularization (physics)Nonlinear opticsFOS: Physical sciencesTransonicNonlinear Sciences::Pattern Formation and SolitonsAtomic and Molecular Physics and OpticsOptics (physics.optics)Physics - Optics
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Shape design optimization in 2D aerodynamics using Genetic Algorithms on parallel computers

1996

Publisher Summary This chapter presents two Shape Optimization problems for two dimensional airfoil designs. The first one is a reconstruction problem for an airfoil when the velocity of the flow is known on the surface of airfoil. The second problem is to minimize the shock drag of an airfoil at transonic regime. The flow is modeled by the full potential equations. The discretization of the state equation is done using the finite element method and the resulting non-linear system of equations is solved by using a multi-grid method. The non-linear minimization process corresponding to the shape optimization problems are solved by a parallel implementation of a genetic algorithm (GA). Some n…

Physics::Fluid DynamicsAirfoilOptimal designMathematical optimizationDiscretizationApplied mathematicsShape optimizationAerodynamicsTransonicFinite element methodMathematicsSequential quadratic programming
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Optimal design for transonic flows

1991

The feasibility of finite element and mathematical programming methods for finding an optimal shape for an symmetric airfoil in case of transonic flow is studied. The state problem is solved using multigrid-technique. Numerical examples are given.

Physics::Fluid DynamicsAirfoilOptimal designMultigrid methodComputer scienceApplied mathematicsState (computer science)TransonicFinite element method
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