Author: Stanley Jay MileyPublisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 362
Book Description
An Analysis of the Design of Airfoil Sections for Low Reynolds Numbers
Author: Stanley Jay MileyPublisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 362
Book Description
Low Reynolds Number Aerodynamics
Author: Thomas J. MuellerPublisher: Springer Science & Business Media
ISBN: 3642840108
Category : Science
Languages : en
Pages : 456
Book Description
Current interest in a variety of low Reynolds number applications has focused attention on the design and evaluation of efficient airfoil sections at chord Reynolds numbers from about 100,000 to about 1,000,000. These applications include remotely piloted vehicles (RPVs) at high altitudes, sailplanes, ultra-light man-carrying/man powered aircraft, mini-RPVs at low altitudes and wind turbines/propellers. The purpose of this conference was to bring together those researchers who have been active in areas closely related to this subject. All of the papers presented are research type papers. Main topics are: Airfoil Design and Analysis, Computational Studies, Stability and Transition, Laminar Separation Bubble, Steady and Unsteady Wind Tunnel Experiments and Flight Experiments.
Summary of Low Speed Airfoil Data
Author: Michael S. SeligPublisher: Soartech
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 320
Book Description
Low Reynolds Number Aerodynamics
Author: Thomas J. MuellerPublisher: Springer
ISBN: 9783642840111
Category : Science
Languages : en
Pages : 451
Book Description
Current interest in a variety of low Reynolds number applications has focused attention on the design and evaluation of efficient airfoil sections at chord Reynolds numbers from about 100,000 to about 1,000,000. These applications include remotely piloted vehicles (RPVs) at high altitudes, sailplanes, ultra-light man-carrying/man powered aircraft, mini-RPVs at low altitudes and wind turbines/propellers. The purpose of this conference was to bring together those researchers who have been active in areas closely related to this subject. All of the papers presented are research type papers. Main topics are: Airfoil Design and Analysis, Computational Studies, Stability and Transition, Laminar Separation Bubble, Steady and Unsteady Wind Tunnel Experiments and Flight Experiments.
Airfoil Design and Data
Author: Richard EpplerPublisher: Springer Science & Business Media
ISBN: 3662026465
Category : Technology & Engineering
Languages : en
Pages : 569
Book Description
This detailed book describes a procedure for the design and analysis of subsonic airfoils. Contains 116 new airfoils for a wide range of Reynolds numbers and application requirements, including the input data for the computer code.
Low Reynolds Number
Author: Mustafa Serdar GençPublisher: BoD – Books on Demand
ISBN: 9535104926
Category : Science
Languages : en
Pages : 176
Book Description
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.
AGARDograph
Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and DevelopmentPublisher:
ISBN: 9789283514862
Category : Aerodynamics
Languages : en
Pages :
Book Description
A Computer Program for the Design and Analysis of Low-speed Airfoils
Author: Richard A. EpplerPublisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 152
Book Description
Airfoils at Low Speeds
Author: Michael S. SeligPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 424
Book Description
The Design of Single Slotted-flapped Airfoil Sections for Low Reynolds Numbers
Author: Lawrence A. SchienbeinPublisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 0
Book Description
The problems associated with the design of a slotted-flap airfoil for high lift and low drag at low Reynolds 6 numbers (-10 ) were investigated and a single slotted-flap airfoil was designed using a simplified design technique. A basic design philosophy was developed; the main points being the proper choice of the basic airfoil section and the modification of the flap section to achieve the desired loading. The maximum' lift coefficient for low drag was determined by the onset of flow separation on the main section while the flap was designed to remain unstalled. The effects of the boundary layer on the lift and the pressure distribution were accounted for by a camber change related to the calculated boundary layer displacement thicknesses. A maximum usable lift coefficient of 2 was found for the slotted-flap airfoil designed in the course of the project.