نتایج جستجو برای: aeroelasticity

تعداد نتایج: 216  

Journal: :Journal of Fluids and Structures 2022

Blade-to-blade variations, known as mistuning, significantly affect the turbomachinery aeroelastic performance. Typically mistuning is observed to be beneficial for flutter stability but detrimental forced response. In some unconventional cases however, may even result in a benefit response reported by researchers. Many previous studies indicated that neglecting mistuning-induced changes aerody...

Journal: :International Journal of Modern Physics: Conference Series 2012

Journal: :Proceedings of Higher Educational Institutions. Маchine Building 2020

2010
Samy Missoum Philip Beran

This paper introduces a methodology for the reliability-based design optimization of systems with nonlinear aeroelastic constraints. The approach is based on the construction of explicit flutter and subcritical limit cycle oscillation boundaries in terms of deterministic and random design variables. The boundaries are constructed using a support vector machine that provides a way to efficiently...

2009
Weihua Su Carlos E. S. Cesnik

This paper presents a study on the coupled aeroelastic/flight dynamic stability and gust response of a blendedwing-body aircraft that derives from the U.S. Air Force’s High Lift-Over-Drag Active (HiLDA) wing experimental model. An effective method is used to model very flexible blended-wing-body vehicles based on a low-order aeroelastic formulation that is capable of capturing the important str...

2008
Satish Kumar Chimakurthi Jian Tang Rafael Palacios Carlos E. S. Cesnik Wei Shyy

Due to their small size and flight regime, coupling of aerodynamics, structural dynamics, and flight dynamics is critical for Micro Aerial Vehicles. This paper presents a computational framework for simulating structural models of varied fidelity and a Navier-Stokes solver, aimed at simulating flapping and flexible wings. The structural model utilizes either (i) the in-house developed UM/NLABS,...

2007
Jack J. McNamara Peretz P. Friedmann

Three time-domain damping/frequency/flutter identification techniques are discussed; namely, the moving-block approach, the least-squares curve-fitting method, and a system-identification technique using an autoregressive moving-average model of the aeroelastic system. These methods are evaluated for use with time-intensive computational aeroelastic simulations, represented by the aeroelastic t...

2012
Drishtysingh Ramdenee Adrian Ilinca Sorin Minea

With roller coaster traditional fuel prices and ever increasing energy demand, wind energy has known significant growth over the last years. To pave the way for higher efficiency and profitability of wind turbines, advances have been made in different aspects related to this technology. One of these has been the increasing size of wind turbines, thus rendering the wind blades gigantic, lighter ...

نمودار تعداد نتایج جستجو در هر سال

با کلیک روی نمودار نتایج را به سال انتشار فیلتر کنید