نتایج جستجو برای: tip wing losing

تعداد نتایج: 69399  

2013
Bo Cheng Sanjay P. Sane Giovanni Barbera Daniel R. Troolin Tyson Strand Xinyan Deng

We investigated the three-dimensional vorticity dynamics of the flows generated by revolving wings using a volumetric 3-component velocimetry system. The threedimensional velocity and vorticity fields were represented with respect to the base axes of rotating Cartesian reference frames, and the second invariant of the velocity gradient was evaluated and used as a criterion to identify two core ...

Journal: :Journal of the Korean Society for Aeronautical & Space Sciences 2013

Journal: :Journal of the Japan Society for Aeronautical and Space Sciences 1992

Journal: :TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B 2011

2007
L. F. Gonzalez J. Périaux K. Srinivas E. J. Whitney

Asynchronous Parallel Evolutionary Algorithms (HAPEAs) have shown to be robust as they require no derivatives or gradients of the objective function, have the capability of finding globally optimum solutions amongst many local optima, can be executed asynchronously in parallel and adapted easily to arbitrary solver codes without major modifications. The application of the methodology is illustr...

2004
CHRISTOPHER ASARO R. SCOTT CAMERON JOHN T. NOWAK DONALD M. GROSMAN JIMMY O. SECKINGER C. WAYNE BERISFORD

The use of pheromone trap catches to reliably predict damage by the Nantucket pine tipmoth,Rhyacionia frustrana (Comstock), in loblolly pine (Pinus taedaL.)plantationswouldprovide forest managers with a valuable integrated pest management tool. At 17 sites throughout four states in the southern United States, in areas where R. frustrana has four annual generations, adult moths were monitored th...

2011
Matt Shields Kamran Mohseni

The growing interest in micro aerial vehicles has brought attention to the need for an improved understanding of the aerodynamics of low-aspect-ratio wings at lowReynolds numbers. In this study, flat plate wings with rectangular and tapered planforms were fabricated with aspect ratios of 0.75, 1, 1.5, and 3, and the aerodynamic loading was measured at Reynolds numbers between 5 10 and 1 10. Sur...

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