This report shows how the actual performance of an airplane varies with air temperature when the pressure is held constant. This leads to comparatively simple methods of reducing observed data to standard conditions. The new methods which may be considered exact for all practical purposes, have been used by the Navy Department for about a year, with very satisfactory results. The report also contains a brief historical review of the important papers which have been published on the subject of performance reduction, and traces the development of the standard atmosphere. (author
Tests were conducted at the altitude laboratory erected at the Bureau of Standards for the National ...
The results of an investigation to determine the pressures in the open cockpit of a Vought VE-7 airp...
A generalized analysis of a pressure-jet powerplant has been made. The effect of changes i n ambien...
This report shows how the actual performance of an airplane varies with air temperature when the pre...
This report contains a brief study of the variation of engine power with temperature and pressure. T...
This report discusses the relation between the temperature of the air at the entrance to the carbure...
This report was prepared at the request of the National Advisory Committee for Aeronautics and discu...
As an airplane rises to high altitudes the decrease in the density and the temperature of the air ha...
This report is based upon an analysis of a large number of airplane-engine tests. It contains the re...
This report deals with the results of a test made upon a B. M. W. Engine in the altitude chamber of ...
Among other factors which affect the horsepower of an airplane engine are the atmospheric pressure, ...
This report presents some results obtained during an investigation to determine the effect of high i...
The pressure in the cabin of a Fairchild cabin monoplane wa surveyed in flight, and was found to dec...
This report is a study of the results obtained from a large number of test of an Hispano-Suiza airpl...
The procedure for obtaining air-speed and rate-of-climb measurements in performance tests of airship...
Tests were conducted at the altitude laboratory erected at the Bureau of Standards for the National ...
The results of an investigation to determine the pressures in the open cockpit of a Vought VE-7 airp...
A generalized analysis of a pressure-jet powerplant has been made. The effect of changes i n ambien...
This report shows how the actual performance of an airplane varies with air temperature when the pre...
This report contains a brief study of the variation of engine power with temperature and pressure. T...
This report discusses the relation between the temperature of the air at the entrance to the carbure...
This report was prepared at the request of the National Advisory Committee for Aeronautics and discu...
As an airplane rises to high altitudes the decrease in the density and the temperature of the air ha...
This report is based upon an analysis of a large number of airplane-engine tests. It contains the re...
This report deals with the results of a test made upon a B. M. W. Engine in the altitude chamber of ...
Among other factors which affect the horsepower of an airplane engine are the atmospheric pressure, ...
This report presents some results obtained during an investigation to determine the effect of high i...
The pressure in the cabin of a Fairchild cabin monoplane wa surveyed in flight, and was found to dec...
This report is a study of the results obtained from a large number of test of an Hispano-Suiza airpl...
The procedure for obtaining air-speed and rate-of-climb measurements in performance tests of airship...
Tests were conducted at the altitude laboratory erected at the Bureau of Standards for the National ...
The results of an investigation to determine the pressures in the open cockpit of a Vought VE-7 airp...
A generalized analysis of a pressure-jet powerplant has been made. The effect of changes i n ambien...