Skip to main content
Article thumbnail
Location of Repository

Further tests of a laminar flow swept wing with boundary layer control by suction

By R. R. Landeryou and P. G. Porter

Abstract

Prepared under Ministry of Aviation contract No. KD/18/09/CB63(a

Publisher: Cranfield University, College of Aeronautics
Year: 1966
OAI identifier: oai:dspace.lib.cranfield.ac.uk:1826/5661
Provided by: Cranfield CERES

Suggested articles


To submit an update or takedown request for this paper, please submit an Update/Correction/Removal Request.