Obtaining lift and induced drag using a wake integration technique applied to PTV studies of a NACA 0015 wing with gurney flap
11th, International symposium on flow visualization ; 2004 ; Notre Dame, IN
2004-01-01
258 pages
Also known as ISFV11. Held on CD-ROM
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
NACA 0015 wing pressure and trailing vortex measurements
NTRS | 1991
|Gurney Flap Scaling for Optimum Lift-to-Drag Ratio
AIAA | 1997
|Gurney Flap Scaling for Optimum Lift-to-Drag Ratio (TN)
Online Contents | 1997
|