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Preliminary Flight Tests of the N.A.C.A. Roots Type Aircraft Engine SuperchargerAn investigation of the suitability of the N.A.C.A. Roots type aircraft engine supercharger to flight-operating conditions, as determined the effects of the use of the supercharger upon engine operation and airplane performance, is described in this report. Attention was concentrated on the operation of the engine-supercharger unit and on the improvement of climbing ability; some information concerning high speeds at altitude was obtained. The supercharger was found to be satisfactory under flight-operating conditions. Although two failures occurred during the tests, the causes of both were minor and have been eliminated. Careful examination of the engines revealed no detrimental effects which could be attributed to supercharging. Marked improvements in climbing ability and high speeds at altitude were effected. It was also found that the load which could be carried to a given moderate or high altitude in a fixed time was considerably augmented. A slight sacrifice of low-altitude performance was necessitated, however, by the use of a fixed-pitch propeller. From a consideration of the very satisfactory flight performance of the Roots supercharger and of its inherent advantages, it is concluded that this type is particularly attractive for use in certain classes of commercial airplanes and in a number of military types.
Document ID
19930091331
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gardiner, Arthur W
Reid, Elliott G
Date Acquired
September 6, 2013
Publication Date
January 1, 1928
Report/Patent Number
NACA-TR-263
Report Number: NACA-TR-263
Accession Number
93R20621
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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