INFLUENCE OF OSCILLATION AMPLITUDE AND MACH NUMBER ON THE UNSTEADY TRANSITION ON A PITCHING ROTOR BLADE AIRFOIL
International annual forum; 69th, American Helicopter Society; Vertical Flight Technical Society ; 2013 ; Phoenix, AZ
2013-01-01
13 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Experimental Investigation of Unsteady Transition on a Pitching Rotor Blade Airfoil
Tema Archiv | 2014
|Unsteady Flow Past a Two-dimensional Airfoil Undergoing Large-amplitude Pitching Motion
British Library Conference Proceedings | 2000
|