An Experimental and Computational Study of Low Re Number Transitional Flows over an Aerofoil with Leading Edge Slat
CONFERENCE; 8th, AIAA aviation technology, integration and operations ; 2008 ; Anchorage, Alaska
2008-01-01
16 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2008
|Flow over an aerofoil without and with a leading-edge slat at a transitional Reynolds number
Online Contents | 2009
|Flow over an aerofoil without and with a leading-edge slat at a transitional Reynolds number
SAGE Publications | 2009
|