Numerical Simulation of a Pitching NACA 0012 Airfoil
INTERNATIONAL CONGRESS; 22nd, International Council of the Aeronautical Sciences ; 2000 ; Harrogate
01.01.2000
7.7.3
HELD ON CD-ROM
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Leading-Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil
Online Contents | 2013
|LEADING EDGE FLOW STRUCTURE OF A DYNAMICALLY PITCHING NACA 0012 AIRFOIL
British Library Conference Proceedings | 2011
|