Investigation carried out at Pilotless Aircraft Research Station, Wallops Island, Va.
Flight investigation at mach numbers from 0.6 to 1.7 to determine drag and base pressures on blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift
NACA -- Tech Note
1955
19 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Drag Force Balance of a Blunt and Divergent Trailing-Edge Airfoil
Online Contents | 2010
|Analysis of Blunt Trailing Edge Airfoils
AIAA | 2003
|