Theoretical solution of problem; transformation function for bi-linear profile; calculation of force components and moments. (See also - discussion p 478)
Effect of hinged flap on aerodynamic characteristics of an airfoil
Cinquieme Congres International de la Navigation Aerienne
5th International Congress of Avigation ; 1930
1930
14 pages
1 Fig.
Aufsatz (Konferenz)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
AERODYNAMIC DEVICE WITH HINGED FLAP (VERSIONS) AND METHOD OF DEPLOYING HINGED FLAP
Europäisches Patentamt | 2017
|Engineering Index Backfile | 1950
|Aerodynamic characteristics of NACA 4412 airfoil sction with flap
Online Contents | 2009
|