AN EXPERIMENTAL AND COMPUTATIONAL STUDY OF LOW RE NUMBER TRANSITIONAL FLOWS OVER AN AEROFOIL WITH LEADING EDGE SLAT
International congress; 26th, International Council of the Aeronautical Sciences; 8th AIAA Aviation Technology, Integration, and Operations (ATIO) ; 2008 ; Anchorage, Alaska
2008-01-01
79 pages
Held on CD-ROM. Also Known as ICAS 2008; Held in e-store (RMS)
Conference paper
English
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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
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