Add to ORKGThe performance of an exhaust turbine driving a supercharger is investigated by means of a sample calculation based on reasonable assumptions for the purpose of determining whether the assumed installation is stable with respect to changes in the mass of gas handled, boost pressure, etc. The arrangement was found to be stable throughout the entire range of operation. The method developed can be generally applied
PaperPg. 90-104.The transformation between work and other forms of energy is accomplished in turboma...
A study was made of the performance of a jet-propulsion system composed of an engine-driven blower, ...
A computerized method which utilizes the engine performance data is described. The method estimates ...
Discussed here are the principles and operation of aircraft engine superchargers used to maintain an...
Charts are presented for computing thrust, fuel consumption, and other performance values of a turbo...
In what follows the question of the number and geometrical arrangement of the cylinders so important...
Convenient charts are presented for computing the thrust, fuel consumption, and other performance va...
Experiments were carried out using a special engine with small glass windows and a stroboscope to re...
In terminating the study of the adaptation of the engine to the airplane, we will examine the proble...
Calculations based on dynamometer test-stand data obtained on an 18-cylinder radial engine were made...
Simple and accurate calculations are made of the flow process in a continuous compressorless Lorin j...
PaperPg. 90-104.The transformation between work and other forms of energy is accomplished in turboma...
The Rateau supercharger investigated had, under normal operating conditions, an adiabatic efficiency...
In part one of this report are presented the theoretical performance curves of an airplane engine eq...
Various methods of providing compressor-capacity and pressure-ratio control in the gas-generator typ...
PaperPg. 90-104.The transformation between work and other forms of energy is accomplished in turboma...
A study was made of the performance of a jet-propulsion system composed of an engine-driven blower, ...
A computerized method which utilizes the engine performance data is described. The method estimates ...
Discussed here are the principles and operation of aircraft engine superchargers used to maintain an...
Charts are presented for computing thrust, fuel consumption, and other performance values of a turbo...
In what follows the question of the number and geometrical arrangement of the cylinders so important...
Convenient charts are presented for computing the thrust, fuel consumption, and other performance va...
Experiments were carried out using a special engine with small glass windows and a stroboscope to re...
In terminating the study of the adaptation of the engine to the airplane, we will examine the proble...
Calculations based on dynamometer test-stand data obtained on an 18-cylinder radial engine were made...
Simple and accurate calculations are made of the flow process in a continuous compressorless Lorin j...
PaperPg. 90-104.The transformation between work and other forms of energy is accomplished in turboma...
The Rateau supercharger investigated had, under normal operating conditions, an adiabatic efficiency...
In part one of this report are presented the theoretical performance curves of an airplane engine eq...
Various methods of providing compressor-capacity and pressure-ratio control in the gas-generator typ...
PaperPg. 90-104.The transformation between work and other forms of energy is accomplished in turboma...
A study was made of the performance of a jet-propulsion system composed of an engine-driven blower, ...
A computerized method which utilizes the engine performance data is described. The method estimates ...