Wind tunnel results are corrected for model or airfoil by measurements of lift, etc, with and without dummy supports fitted; it is useful to have some independent check by direct calculation on amount of interference to be expected; theory for rectangular airfoil.
Strut interference on aerofoil
Aircraft Eng
Aircraft Engineering ; 28 , n 332
1956
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Strut Interference on an Aerofoil
Emerald Group Publishing | 1956
|Tema Archive | 2006
|