NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Performance of Maybach 300-horsepower airplane engineThis report contains the results of a test made upon a Maybach Engine in the altitude chamber of the Bureau of Standards, where controlled conditions of temperature and pressure can be made the same as those of the desired altitude. The results of this test lead to the following conclusions: from the standpoint of thermal efficiency the full-load performance of the engine is excellent at densities corresponding to altitudes up to and including 15,000 feet. The brake mean effective pressure is rather low even at wide-open throttle. This tends to give a high weight per horsepower, in as much as the weight of many engine parts is governed by the size rather than the power of the engine. At part load the thermal efficiency of the engine is low. Judged on a basis of performance the engine's chief claim to interest would appear to lie in the carburetor design, which is largely responsible excellent full-load efficiency and for its poor part-load efficiency.
Document ID
19930091199
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sparrow, S W
Date Acquired
September 6, 2013
Publication Date
January 1, 1923
Report/Patent Number
NACA-TR-134
Report Number: NACA-TR-134
Accession Number
93R20489
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available