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Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications

Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications
Author: Thomas J. Mueller
Publisher: AIAA
Total Pages: 614
Release: 2001
Genre: Aerodynamics
ISBN: 9781600864469

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This title reports on the latest research in the area of aerodynamic efficency of various fixed-wing, flapping wing, and rotary wing concepts. It presents the progress made by over fifty active researchers in the field.


Parallel Computational Fluid Dynamics 2006

Parallel Computational Fluid Dynamics 2006
Author: Jang-Hyuk Kwon
Publisher: Elsevier
Total Pages: 320
Release: 2007-09-12
Genre: Computers
ISBN: 0080550045

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The proceedings from Parallel CFD 2006 covers all aspects of parallel computings and its applications. Although CFD is one of basic tools for design procedures to produce machineries, such as automobiles, ships, aircrafts, etc., large scale parallel computing has been realized very recently, especially for the manufactures. Various applications in many areas could be experienced including acoustics, weather prediction and ocean modeling, flow control, turbine flow, fluid-structure interaction, optimization, heat transfer, hydrodynamics. - Report on current research in the field in an area which is rapidly changing - Subject is important to all interested in solving large fluid dynamics problems - Interdisciplinary activity. Contributions include scientists with a variety of backgrounds


An Introduction to Flapping Wing Aerodynamics

An Introduction to Flapping Wing Aerodynamics
Author: Wei Shyy
Publisher: Cambridge University Press
Total Pages: 321
Release: 2013-08-19
Genre: Technology & Engineering
ISBN: 1107067987

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This is an ideal book for graduate students and researchers interested in the aerodynamics, structural dynamics and flight dynamics of small birds, bats and insects, as well as of micro air vehicles (MAVs), which present some of the richest problems intersecting science and engineering. The agility and spectacular flight performance of natural flyers, thanks to their flexible, deformable wing structures, as well as to outstanding wing, tail and body coordination, is particularly significant. To design and build MAVs with performance comparable to natural flyers, it is essential that natural flyers' combined flexible structural dynamics and aerodynamics are adequately understood. The primary focus of this book is to address the recent developments in flapping wing aerodynamics. This book extends the work presented in Aerodynamics of Low Reynolds Number Flyers (Shyy et al. 2008).


Computational Fluid Dynamics 2000

Computational Fluid Dynamics 2000
Author: Nobuyuki Satofuka
Publisher: Springer Science & Business Media
Total Pages: 807
Release: 2012-12-06
Genre: Science
ISBN: 3642565352

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These proceedings contain a selection of refereed contributions as a source of reference for all those interested in the state of the art in computational fluid dynamics. The conference brings together physicists, mathematicians and engineers to review and share recent advances in the field.


AIAA Journal

AIAA Journal
Author: American Institute of Aeronautics and Astronautics
Publisher:
Total Pages: 530
Release: 2008
Genre: Aeronautics
ISBN:

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Applied Mechanics Reviews

Applied Mechanics Reviews
Author:
Publisher:
Total Pages: 620
Release: 1996
Genre: Mechanics, Applied
ISBN:

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Unsteady Aerodynamics of a Flapping Airfoil

Unsteady Aerodynamics of a Flapping Airfoil
Author: Sunetra Sarkar
Publisher: LAP Lambert Academic Publishing
Total Pages: 204
Release: 2010-03
Genre:
ISBN: 9783838347592

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This book analyzes the unsteady, viscous flow-field of an oscillating airfoil. This has ramifications on understanding the flapping flight of natural biological systems like fishes and invertebrates. It also helps towards a better aerodynamic design and understanding of flapping types MAVs. The flow-field simulation is performed with a grid-free Lagrangian particle based solver using vorticity particles. An examination of the unsteady aerodynamic load and the qualitative wake structures are done for airfoils undergoing pitch and plunge oscillations. The propulsive behavior is investigated at medium to high frequency ranges for different relevant parameters. These are amplitude of oscillation, mean angle of attack, and rotational axis location. Asymmetric sinusoidal motions are also examined. Dynamic stall is another important aspect of unsteady aerodynamics that airfoils and wings experience during their time dependent movement at large angles of attack. Insects use this phenomenon to increase the aerodynamic loads during their large angle flapping maneuvers. This aspect is also studied in this book.