In this report it will be seen that the piston speed - as, moreover, any other speed, such as bearing velocity - must be independent of the quantity dimensions and must be a representative quantity similar to the high speed and the specific weight per horsepower
The present paper describes a device whereby rapid flame movement within an internal-combustion engi...
The tests upon which this report is based were made at the Bureau of Standards between October 1919 ...
The air flow in combustion chambers is divided into three fundamental classes - induced, forced, and...
The power and heat-stress conditions of geometrically similar engines are discussed. The advantages ...
Comparing the results of the calculations for computing the mean pressure of an aviation engine for ...
Three high-speed semi-diesel engines are examined through the use of indicator diagrams. Different f...
It is extremely important in building aircraft engines to determine the requisite cylinder dimension...
This adaptation of a Russian report reveals the effect of maximum cross section of an engine as well...
Experiments were carried out using a special engine with small glass windows and a stroboscope to re...
Data are presented to show the effects of inlet-air pressure, inlet-air temperature, and compression...
An analytical investigation was made of the performance of isolated ram-jet engines in the flight Ma...
Tests made on a Curtiss D-12 engine in the Altitude Laboratory at the Bureau of Standards show the f...
The viewpoints are discussed, according to which the scavenging of two-stroke-cycle engines can be e...
An investigation was conducted to correlate the knock limited performance of flight and single-cylin...
This report presents the results of tests made on three sizes of roots type aircraft engine supercha...
The present paper describes a device whereby rapid flame movement within an internal-combustion engi...
The tests upon which this report is based were made at the Bureau of Standards between October 1919 ...
The air flow in combustion chambers is divided into three fundamental classes - induced, forced, and...
The power and heat-stress conditions of geometrically similar engines are discussed. The advantages ...
Comparing the results of the calculations for computing the mean pressure of an aviation engine for ...
Three high-speed semi-diesel engines are examined through the use of indicator diagrams. Different f...
It is extremely important in building aircraft engines to determine the requisite cylinder dimension...
This adaptation of a Russian report reveals the effect of maximum cross section of an engine as well...
Experiments were carried out using a special engine with small glass windows and a stroboscope to re...
Data are presented to show the effects of inlet-air pressure, inlet-air temperature, and compression...
An analytical investigation was made of the performance of isolated ram-jet engines in the flight Ma...
Tests made on a Curtiss D-12 engine in the Altitude Laboratory at the Bureau of Standards show the f...
The viewpoints are discussed, according to which the scavenging of two-stroke-cycle engines can be e...
An investigation was conducted to correlate the knock limited performance of flight and single-cylin...
This report presents the results of tests made on three sizes of roots type aircraft engine supercha...
The present paper describes a device whereby rapid flame movement within an internal-combustion engi...
The tests upon which this report is based were made at the Bureau of Standards between October 1919 ...
The air flow in combustion chambers is divided into three fundamental classes - induced, forced, and...