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|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.|
|Appears in Collections:||College of Aeronautics Reports|
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