Numerical Investigation & Performance Comparison of Aerofoil Shapes

ISBN-13: 9786139910304 / Angielski / Miękka / 52 str.

Jaswinder Singh Mehta

Opis

The book is founded on investigating the performance of different aerofoil shapes at varying angles of attack by conducting numerical investigation. The performance of the aerofoil shapes has been evaluated on the basis of the criterion of lift force generation as the aerofoils are designed in such a way that they generate maximum amount of lift. Different plots such as velocity contours and coefficient of lift and coefficient of drag versus different angles of attack have also been plotted for assessing the performance of different aerofoil shapes.

O autorze

Mehta, Jaswinder SinghThe author is working with Panjab University, Chandigarh. His main research interests are in the field of optimization and nanofluid heat transfer and has more than 18 years of teaching experience.