Numerical Study of Limit Cycle Oscillation Using Conventional and Supercritical Airfoils
By:Felipe Manuel Loo
Published on 2008 by
Limit Cycle Oscillation is a type of aircraft wing structural vibration caused by the non-linearity of the system. The objective of this thesis is to provide a numerical study of this aeroelastic behavior. A CFD solver is used to simulate airfoils displaying such an aeroelastic behavior under certain airflow conditions. Two types of airfoils are used for this numerical study, including the NACA64a010 airfoil, and the supercritical NLR 7301 airfoil. The CFD simulation of limit cycle oscillation (LCO) can be obtained by using published flow and structural parameters. Final results from the CFD solver capture LCO, as well as flutter, behaviors for both wings. These CFD results can be obtained by using two different solution schemes, including the Roe and Zha scheme. The pressure coefficient and skin friction coefficient distributions are computed using the CFD results for LCO and flutter simulations of these two airfoils, and they provide a physical understanding of these aeroelastic behaviors.
This Book was ranked at 35 by Google Books for keyword oscillating.
Book ID of Numerical Study of Limit Cycle Oscillation Using Conventional and Supercritical Airfoils's Books is Z76BAQAACAAJ, Book which was written byFelipe Manuel Loohave ETAG "qxNJGyIkRg4"
Book which was published by since 2008 have ISBNs, ISBN 13 Code is and ISBN 10 Code is
Reading Mode in Text Status is false and Reading Mode in Image Status is false
Book which have " Pages" is Printed at BOOK under Category
This Book was rated by Raters and have average rate at ""
This eBook Maturity (Adult Book) status is NOT_MATURE
Book was written in en
eBook Version Availability Status at PDF is falseand in ePub is false
Book Preview
0 komentar:
Posting Komentar