Analysis of lift and pitching moment of airfoil at subsonic speed affected by flap deflection involving flow separation

Authors
CHOI, HANG CHEOLPaul K. Chang
Citation
한국항공우주학회 1982 년도 춘계학술강연회, pp.1 - 7
Keywords
multi-component airfoil; fredholm' s integral equation of second kind; flow separation; singularity distribution
URI
https://pubs.kist.re.kr/handle/201004/112863
Appears in Collections:
KIST Conference Paper > Others
Files in This Item:
There are no files associated with this item.
Export
RIS (EndNote)
XLS (Excel)
XML

qrcode

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.

BROWSE