Add to ORKGReports of tests of a Daimler IVa engine at the test-bench at Friedrichshafen, show that the decrease of power of that engine, at high altitudes, was established, and that the manner of its working when air is supplied at a certain pressure was explained. These tests were preparatory to the installation of compressors in giant aircraft for the purpose of maintaining constant power at high altitudes
In part one of this report are presented the theoretical performance curves of an airplane engine eq...
Engine test results are presented for simulated altitude conditions. A displaced-piston combustion c...
This report contains the results of a test made upon a Maybach Engine in the altitude chamber of the...
Reports of tests of a Daimler IVa engine at the test-bench at Friedrichshafen, show that the decreas...
In terminating the study of the adaptation of the engine to the airplane, we will examine the proble...
Issues and techniques relative to the adaptation of aircraft engines to high altitude flight are dis...
This report is based upon an analysis of a large number of airplane-engine tests. It contains the re...
The National Bureau of Standards tested a 300-horsepower Hispano-Suiza engine to determine the chara...
The rate of change in power of aircraft engines with altitude has been the subject of considerable d...
Among other factors which affect the horsepower of an airplane engine are the atmospheric pressure, ...
This report is based upon engine tests made at the Bureau of Standards during 1920, 1921, 1922, and ...
It became evident during World War I that ever-increasing demands were being placed on the mean powe...
This report deals with the results of a test made upon a B. M. W. Engine in the altitude chamber of ...
This report presents the results of preliminary tests made on the effects of supercharging an air-co...
An investigation of the suitability of the N.A.C.A. Roots type aircraft engine supercharger to fligh...
In part one of this report are presented the theoretical performance curves of an airplane engine eq...
Engine test results are presented for simulated altitude conditions. A displaced-piston combustion c...
This report contains the results of a test made upon a Maybach Engine in the altitude chamber of the...
Reports of tests of a Daimler IVa engine at the test-bench at Friedrichshafen, show that the decreas...
In terminating the study of the adaptation of the engine to the airplane, we will examine the proble...
Issues and techniques relative to the adaptation of aircraft engines to high altitude flight are dis...
This report is based upon an analysis of a large number of airplane-engine tests. It contains the re...
The National Bureau of Standards tested a 300-horsepower Hispano-Suiza engine to determine the chara...
The rate of change in power of aircraft engines with altitude has been the subject of considerable d...
Among other factors which affect the horsepower of an airplane engine are the atmospheric pressure, ...
This report is based upon engine tests made at the Bureau of Standards during 1920, 1921, 1922, and ...
It became evident during World War I that ever-increasing demands were being placed on the mean powe...
This report deals with the results of a test made upon a B. M. W. Engine in the altitude chamber of ...
This report presents the results of preliminary tests made on the effects of supercharging an air-co...
An investigation of the suitability of the N.A.C.A. Roots type aircraft engine supercharger to fligh...
In part one of this report are presented the theoretical performance curves of an airplane engine eq...
Engine test results are presented for simulated altitude conditions. A displaced-piston combustion c...
This report contains the results of a test made upon a Maybach Engine in the altitude chamber of the...