CERES > School of Engineering (SoE) > College of Aeronautics Reports >

Please use this identifier to cite or link to this item: http://dspace.lib.cranfield.ac.uk/handle/1826/7227

Document Type: Report
Title: Measurements of the pressure distribution on swept back wings with trailing edge split flaps: summary of wind tunnel work at the College of Aeronautics 1948 - 50
Authors: Babister, A. W.
Issue Date: Mar-1951
Abstract: This is an interim report giving measurement s that have so far been made of pressure distribution on two untapered wings swept back 45◦, aspect ratio 2 and 4, fitted with both full span and part span trailing edge split flaps. The Reynolds number in these tests was about 0.5x106.
URI: http://dspace.lib.cranfield.ac.uk/handle/1826/7227
Appears in Collections:College of Aeronautics Reports

Files in This Item:

File Description SizeFormat
COA_Report_No_43_MAR_1951.pdf6.14 MBAdobe PDFView/Open

SFX Query

Items in CERES are protected by copyright, with all rights reserved, unless otherwise indicated.