Summary of Low Speed Airfoil Data
Author | : Michael S. Selig |
Publisher | : Soartech |
Total Pages | : 320 |
Release | : 1995 |
Genre | : Technology & Engineering |
ISBN | : |
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Author | : Michael S. Selig |
Publisher | : Soartech |
Total Pages | : 320 |
Release | : 1995 |
Genre | : Technology & Engineering |
ISBN | : |
Author | : Thomas J. Mueller |
Publisher | : AIAA |
Total Pages | : 614 |
Release | : 2001 |
Genre | : Aerodynamics |
ISBN | : 9781600864469 |
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.
Author | : Mustafa Serdar Genç |
Publisher | : BoD – Books on Demand |
Total Pages | : 176 |
Release | : 2012-04-04 |
Genre | : Science |
ISBN | : 9535104926 |
This book reports the latest development and trends in the low Re number aerodynamics, transition from laminar to turbulence, unsteady low Reynolds number flows, experimental studies, numerical transition modelling, control of low Re number flows, and MAV wing aerodynamics. The contributors to each chapter are fluid mechanics and aerodynamics scientists and engineers with strong expertise in their respective fields. As a whole, the studies presented here reveal important new directions toward the realization of applications of MAV and wind turbine blades.
Author | : Michael S. Selig |
Publisher | : |
Total Pages | : 424 |
Release | : 1989 |
Genre | : Aerodynamics |
ISBN | : |
Author | : Hugh W. Coleman |
Publisher | : John Wiley & Sons |
Total Pages | : 404 |
Release | : 2018-04-09 |
Genre | : Technology & Engineering |
ISBN | : 1119417708 |
Helps engineers and scientists assess and manage uncertainty at all stages of experimentation and validation of simulations Fully updated from its previous edition, Experimentation, Validation, and Uncertainty Analysis for Engineers, Fourth Edition includes expanded coverage and new examples of applying the Monte Carlo Method (MCM) in performing uncertainty analyses. Presenting the current, internationally accepted methodology from ISO, ANSI, and ASME standards for propagating uncertainties using both the MCM and the Taylor Series Method (TSM), it provides a logical approach to experimentation and validation through the application of uncertainty analysis in the planning, design, construction, debugging, execution, data analysis, and reporting phases of experimental and validation programs. It also illustrates how to use a spreadsheet approach to apply the MCM and the TSM, based on the authors’ experience in applying uncertainty analysis in complex, large-scale testing of real engineering systems. Experimentation, Validation, and Uncertainty Analysis for Engineers, Fourth Edition includes examples throughout, contains end of chapter problems, and is accompanied by the authors’ website www.uncertainty-analysis.com. Guides readers through all aspects of experimentation, validation, and uncertainty analysis Emphasizes the use of the Monte Carlo Method in performing uncertainty analysis Includes complete new examples throughout Features workable problems at the end of chapters Experimentation, Validation, and Uncertainty Analysis for Engineers, Fourth Edition is an ideal text and guide for researchers, engineers, and graduate and senior undergraduate students in engineering and science disciplines. Knowledge of the material in this Fourth Edition is a must for those involved in executing or managing experimental programs or validating models and simulations.
Author | : Leonard M. Rose |
Publisher | : |
Total Pages | : 28 |
Release | : 1949 |
Genre | : Aerofoils |
ISBN | : |
A faired, double-wedge airfoil section, 4.23 percent thick, was investigated with plain nose and trailing-edge flaps. The nose flap was 0.16 chord of the airfoil and the trailing-edge flap was 0.25 chord of the airfoil. Section lift, drag, and pitching-momnet data are presented for a Reynolds number of 5,800,000 which corresponded to a Mach number of 0.17.
Author | : Wei Shyy |
Publisher | : Cambridge University Press |
Total Pages | : 0 |
Release | : 2011-04-28 |
Genre | : Technology & Engineering |
ISBN | : 9780521204019 |
Low Reynolds number aerodynamics is important to a number of natural and man-made flyers. Birds, bats, and insects have been of interest to biologists for years, and active study in the aerospace engineering community, motivated by interest in micro air vehicles (MAVs), has been increasing rapidly. The primary focus of this book is the aerodynamics associated with fixed and flapping wings. The book consider both biological flyers and MAVs, including a summary of the scaling laws-which relate the aerodynamics and flight characteristics to a flyer's sizing on the basis of simple geometric and dynamics analyses, structural flexibility, laminar-turbulent transition, airfoil shapes, and unsteady flapping wing aerodynamics. The interplay between flapping kinematics and key dimensionless parameters such as the Reynolds number, Strouhal number, and reduced frequency is highlighted. The various unsteady lift enhancement mechanisms are also addressed, including leading-edge vortex, rapid pitch-up and rotational circulation, wake capture, and clap-and-fling.
Author | : Cameron Tropea |
Publisher | : Springer Science & Business Media |
Total Pages | : 1570 |
Release | : 2007-10-09 |
Genre | : Science |
ISBN | : 3540251413 |
Accompanying DVD-ROM contains ... "all chapters of the Springer Handbook."--Page 3 of cover.
Author | : Vassilis Theofilis |
Publisher | : Springer |
Total Pages | : 281 |
Release | : 2015-01-03 |
Genre | : Technology & Engineering |
ISBN | : 3319062603 |
This book contains the outcome of the international meeting on instability, control and noise generated by massive flow separation that was organized at the Monash Center, in Prato, Italy, September 4-6, 2013. The meeting served as the final review of the EU-FP7 Instability and Control of Massively Separated Flows Marie Curie travel grant and was supported by the European Office of Aerospace Research and Development. Fifty leading specialists from twelve countries reviewed the progress made since the 50s of the last century and discussed modern analysis techniques, advanced experimental flow diagnostics and recent developments in active flow control techniques from the incompressible to the hypersonic regime. Applications involving massive flow separation and associated instability and noise generation mechanisms of interest to the aeronautical, naval and automotive industries have been addressed from a theoretical, numerical or experimental point of view, making this book a unique source containing the state-of-the-art in separated flow instability and its control.
Author | : Csaba Hefler |
Publisher | : Cambridge University Press |
Total Pages | : 104 |
Release | : 2021-05-27 |
Genre | : Technology & Engineering |
ISBN | : 110887522X |
Insect-scale flapping wing flight vehicles can conduct environmental monitoring, disaster assessment, mapping, positioning and security in complex and challenging surroundings. To develop bio-inspired flight vehicles, systematic probing based on the particular category of flight vehicles is needed. This Element addresses the aerodynamics, aeroelasticity, geometry, stability and dynamics of flexible flapping wings in the insect flight regime. The authors highlight distinct features and issues, contrast aerodynamic stability between rigid and flexible wings, present the implications of the wing-aspect ratio, and use canonical models and dragonflies to elucidate scientific insight as well as technical capabilities of bio-inspired design.