To read this content please select one of the options below:

Foreign Research Progress: Translations issued by the N.A.C.A

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 April 1943

17

Abstract

Having accumulated various wind‐tunnel data on suction‐flap aerofoils, the A.V.A. decided to test the theory on an actual aeroplane in flight.

Citation

(1943), "Foreign Research Progress: Translations issued by the N.A.C.A", Aircraft Engineering and Aerospace Technology, Vol. 15 No. 4, pp. 113-113. https://doi.org/10.1108/eb031010

Publisher

:

MCB UP Ltd

Copyright © 1943, MCB UP Limited

Related articles