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Practical Tests with the "auto Control Slot." Part II : DiscussionFor some time the D.V.L. has been investigating the question of applicability of Handley Page slotted wings to German airplanes. Comparitive gliding tests were made with open and closed slots on an Albatros L 75 airplane equipped with the Handley Page "auto control slots." This investigation served to determine the effect of the auto control slot on the properties and performances of airplanes at large angles of attack. The most important problems were whether the angle of glide at small angles of attack can be increased by the adoption of the auto control slot and, in particular, as to whether the flight characteristics at large angles of attack are improved thereby and equilibrium in gliding flight is guaranteed even at larger than ordinary angles of attack.
Document ID
19930094822
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lachmann, G
Date Acquired
September 6, 2013
Publication Date
November 1, 1930
Report/Patent Number
NACA-TM-594
Report Number: NACA-TM-594
Accession Number
93R23742
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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