Among other factors which affect the horsepower of an airplane engine are the atmospheric pressure, and consequently the altitude at which the engine is working, and the compression ratio, or cylinder volume divided by clearance volume. The tests upon which this report is based were selected from a large number of runs made during the intercomparison of various gasolines to determine the variation of horsepower with altitude at three different compression ratios. The test results and conclusions are presented in this report
Report presents the summation of results obtained in the testing of fuels of various compositions an...
This report presents some results obtained during an investigation to determine the effect of high i...
The object of this investigation was to determine the effect of increasing the carburetor pressures ...
Among other factors which affect the horsepower of an airplane engine are the atmospheric pressure, ...
This report discusses the relation between the temperature of the air at the entrance to the carbure...
This report is based upon engine tests made at the Bureau of Standards during 1920, 1921, 1922, and ...
This report is based upon an analysis of a large number of airplane-engine tests. It contains the re...
From tests made in the altitude chamber of the Bureau of Standards, it was found that the effect of ...
This report deals with the results of a test made upon a B. M. W. Engine in the altitude chamber of ...
The rate of change in power of aircraft engines with altitude has been the subject of considerable d...
This report contains the results of a test made upon a Maybach Engine in the altitude chamber of the...
This report contains a brief study of the variation of engine power with temperature and pressure. T...
These notes are intended to furnish practical and general data on the effect of altitude on engine p...
This report is a study of the results obtained from a large number of test of an Hispano-Suiza airpl...
Tests were conducted at the altitude laboratory erected at the Bureau of Standards for the National ...
Report presents the summation of results obtained in the testing of fuels of various compositions an...
This report presents some results obtained during an investigation to determine the effect of high i...
The object of this investigation was to determine the effect of increasing the carburetor pressures ...
Among other factors which affect the horsepower of an airplane engine are the atmospheric pressure, ...
This report discusses the relation between the temperature of the air at the entrance to the carbure...
This report is based upon engine tests made at the Bureau of Standards during 1920, 1921, 1922, and ...
This report is based upon an analysis of a large number of airplane-engine tests. It contains the re...
From tests made in the altitude chamber of the Bureau of Standards, it was found that the effect of ...
This report deals with the results of a test made upon a B. M. W. Engine in the altitude chamber of ...
The rate of change in power of aircraft engines with altitude has been the subject of considerable d...
This report contains the results of a test made upon a Maybach Engine in the altitude chamber of the...
This report contains a brief study of the variation of engine power with temperature and pressure. T...
These notes are intended to furnish practical and general data on the effect of altitude on engine p...
This report is a study of the results obtained from a large number of test of an Hispano-Suiza airpl...
Tests were conducted at the altitude laboratory erected at the Bureau of Standards for the National ...
Report presents the summation of results obtained in the testing of fuels of various compositions an...
This report presents some results obtained during an investigation to determine the effect of high i...
The object of this investigation was to determine the effect of increasing the carburetor pressures ...