نتایج جستجو برای: lift coefficient

تعداد نتایج: 180477  

Journal: :The Journal of experimental biology 2009
Paul W Weber Laurens E Howle Mark M Murray Frank E Fish

Cetaceans (whales, dolphins and porpoises) have evolved flippers that aid in effective locomotion through their aquatic environments. Differing evolutionary pressures upon cetaceans, including hunting and feeding requirements, and other factors such as animal mass and size have resulted in flippers that are unique among each species. Cetacean flippers may be viewed as being analogous to modern ...

2000
T. N. Pornsin-Sirirak Y. C. Tai H. Nassef C. M. Ho

The unsteady-state aerodynamic performance results of various MEMS-fabricated titanium-alloy wing designs are presented. These wing are tested in a high-quality low-speed wind tunnel with velocity uniformity of 0.5%.. For the first time, we have identified the importance of spanwise stiffness effect in generating the leading edge vortices. These vortices, generated around each wing, cause a low...

2008
S. Andrew Ning Ilan Kroo

Conceptual wing design analysis methods are combined with numerical optimization to find minimum drag wings subject to constraints on lift, weight, pitching moment, and stall speed. Minimum drag tip extensions and winglets are compared using nonlinear optimization. The minimum drag trapezoidal tip device depends on the ratio of the maneuver lift coefficient to the cruise lift coefficient, altho...

Journal: :Journal of applied biomechanics 2011
Daniel A Marinho Antonio J Silva Victor M Reis Tiago M Barbosa Joao P Vilas-Boas Francisco B Alves Leandro Machado Abel I Rouboa

The purpose of this study was to analyze the hydrodynamic characteristics of a realistic model of an elite swimmer hand/forearm using three-dimensional computational fluid dynamics techniques. A three-dimensional domain was designed to simulate the fluid flow around a swimmer hand and forearm model in different orientations (0°, 45°, and 90° for the three axes Ox, Oy and Oz). The hand/forearm m...

Numerical investigation was performed on NACA 0015 which is a symmetric airfoil. Pressure distribution and then lift and drag forces are verified. Changing of ground clearance was a considerable point. Also the angle of attack was changed from 0° to 10°. Pressure coefficient reaches its higher amounts on the wing lower surface when the ground clearance diminishes. Increment of the angle of atta...

Journal: :Journal of sports science & medicine 2009
Daniel A Marinho Abel I Rouboa Francisco B Alves João P Vilas-Boas Leandro Machado Victor M Reis António J Silva

The aim of the present study was to analyze the hydrodynamic characteristics of a true model of a swimmer hand with the thumb in different positions using numerical simulation techniques. A three-dimensional domain was created to simulate the fluid flow around three models of a swimmer hand, with the thumb in different positions: thumb fully abducted, partially abducted, and adducted. These thr...

2007
Won Tae Joe Kunihiko Taira Tim Colonius Douglas G. MacMynowski Gilead Tadmor

Openand closed-loop control of vortex shedding in two-dimensional flow over a flat plate at high angles of attack is numerically investigated at a Reynolds number of 300. Unsteady actuation is modeled as a body force near the leading or trailing edge, and is directed either upstream or downstream. For moderate angles of attack, sinusoidal forcing at the natural shedding frequency results in pha...

2015
H. Bayat M. Majidi M. Bolhasani A. Karbalaie Alilou A. Mirabdolah Lavasani

Unsteady flow and heat transfer from a circular cylinder in cross-flow is studied numerically. The governing equations are solved by using finite volume method. Reynolds number varies in range of 50 to 200; in this range flow is considered to be laminar and unsteady. Al2O3 nanoparticle with volume fraction in range of 5% to 20% is added to pure water. Effects of adding nanoparticle to pure wate...

1960
L F Crabtree

Errata The following corrections should be made to the text: 8, Page is defined as the lift coefficient acting on the complete system but due solely to the rotation of the fla u/?and This is given as the difference between the CL at a given value of the CL with flap fixed (P = 45O). However, this value of C LR still includes the effect of the flap acting as an ordinary flap on the wing through ...

The prediction of aerodynamic characteristics and smart flap of airfoil under the ground effect are carried out by the integration of computational fluid dynamics. Considering different types of beams, a parametric bending profile of a smart flap is designed. Cantilever beam with uniformly varying load with roller support at the free end is considered in here. A pressure-based implicit procedur...

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