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Drag measurements on a Junkers wing section : application of the Betz Method to the results of comparative tests made on a model and on an airplane in flightThe comparison of model tests in flight can be based on the result of such measurements. They are very important from the aerodynamical point of view, as they lead to useful conclusions regarding the behavior of the wing, its best shape and the conformity of theoretical and actual flow. Although there still remains a certain prejudice against such measurements, I have still attempted to make these comparative tests in order to inspire confidence in their reliability.
Document ID
19930090796
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Weidinger, Hanns
Date Acquired
September 6, 2013
Publication Date
September 1, 1927
Report/Patent Number
NACA-TM-428
Report Number: NACA-TM-428
Accession Number
93R20086
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGS - JUNKERS A 20
REYNOLDS LAW
DRAG, PROFILE - MEASUREMENT, MOMENTUM
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