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A Preliminary Study of Airplane PerformanceFlight tests were carried out at the Langley Field laboratory of the NACA, on several airplanes for the purpose of determining their relative performance with the same engine and the same propeller. The method used consisted in flying each airplane on a level course and measuring the airspeed for the whole range of engine revolutions. In general the results show that a small change in the wing section or the wing area has but a slight effect upon the performance, but changes in those parts which cause the structural resistance have a very important effect.
Document ID
19930080901
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Norton, F H
Brown, W G
Date Acquired
September 6, 2013
Publication Date
November 1, 1922
Report/Patent Number
NACA-TN-120
Report Number: NACA-TN-120
Accession Number
93R10191
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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