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A Computational Framework for Low Reynolds Number 3D Flapping Wings Simulations
Computational Framework Low Reynolds Number 3D Flapping Wings Simulations
2015/7/3
This paper describes the work done in the development of a fast and accurate numerical solver for flows around flapping wings at low Reynolds numbers. In the first part, the fi...
Aerodynamics and Flight Control of Flapping Wing Flight Vehicles: A Preliminary Computational Study
Aerodynamics Flight Control Flapping Wing Flight Vehicles Preliminary Computational Study
2015/7/2
The dexterity and gracefulness of winged creatures have captured the imagination of humans for a long time. Insects have evolved sophisticated ight control mechanisms that permit a remarkable range of...
ANALYSIS AND IMPLEMENTATION OF THE GAS-KINETIC BGK SCHEME FOR COMPUTATIONAL GAS DYNAMICS
gas evolution model gas-kinetic BGK schemes entropy condition gas-kinetic Lax±Wendroff ˉux
2015/7/1
Gas-kinetic schemes based on the BGK model are proposed as an alternative evolution model which can cure some of the limitations of current Riemann solvers. To analyse the schemes, simple advection eq...
TIME-INTEGRATION METHODS IN COMPUTATIONAL AER OD YNAMICS
AER OD YNAMICS Integration method
2015/6/18
TIME-INTEGRATION METHODS IN COMPUTATIONAL AER OD YNAMICS。
Computational Investigation of Wings with Miniature Trailing Edge Control Surfaces
Miniature Trailing Control Surfaces Wing
2015/6/18
Miniature trailing edge e ectors (MiTEs) are small
aps (typically 1% to 5% chord)
actuated with de
ection angles near 90 degrees. The small size, combined with little
required power and good cont...
Computational simulation of non-geodesic filament winding of pressure vessel of rocket motor
Filament winding Non-geodesic winding Pressure vessel Motor case Rocket
2010/10/25
The main objective of this work was to accomplish the computational simulation in the software CadWind® of a filament winding for an applied pressure vase to motor rocket. The adopted simulation w...
Computational Investigation of Unsteady Internal Flow in Solid Propellant Rockets
Solid Propellant Rockets Unsteady Compressible Flows
2009/10/14
Unsteady flow in a semi-closed axisymmetric cylindrical channel with steady sidewall mass injection that simulates a model of a solid propellant rocket combustion chamber is studied computationally. P...
W. M. Keck Laboratory for Computational Fluid Dynamics（CFD）, University of Michigan（图）
CFD W. M. Keck Laboratory for Computational Fluid Dynamics University of Michigan 动力学 航空航天基础科学 物理学
2007/12/21
The W. M. Keck Laboratory for Computational Fluid Dynamics (CFD) is located in the Fran鏾is-Xavier Bagnoud Building, home of the Department of Aerospace Engineering in the College of Engineering at the...