Add to ORKGCalculations based on dynamometer test-stand data obtained on an 18-cylinder radial engine were made to determine the improvement in fuel consumption that can be obtained at various altitudes by gearing an exhaust-gas turbine to the engine crankshaft in order to increase the engine-shaft work
In order to insure satisfactory turbine performance under five turbojet-engine operating conditions,...
The Rateau supercharger investigated had, under normal operating conditions, an adiabatic efficiency...
AbstractGas-turbines are widely used to power aero planes because they are light, compact with a hig...
Calculations bawd on dynamometer test-stand data obtained on an 18-cylinder radial engine uxre made ...
An investigation was conducted to obtain fuel-consumption curves for a single-cylinder engine with a...
Calculations based on dynamometer test-stand data obtained on an 18-cylinder radial engine were made...
An analytical investigation was made of a topping cycle aircraft engine system which uses a cryogeni...
This report deals with the results of a test made upon a B. M. W. Engine in the altitude chamber of ...
DVL experimental and analytical work on the cooling of turbine blades by using ram air as the workin...
Small high-speed single-cylinder compression-ignition engines were tested to determine their perform...
Adjustable-stator turbines are applied to turbojet engines and probable performance is compared with...
Discussed here are the principles and operation of aircraft engine superchargers used to maintain an...
A parametric study was performed to determine the performance limits of a rotary combustion engine. ...
In part one of this report are presented the theoretical performance curves of an airplane engine eq...
This report contains the results of a test made upon a Maybach Engine in the altitude chamber of the...
In order to insure satisfactory turbine performance under five turbojet-engine operating conditions,...
The Rateau supercharger investigated had, under normal operating conditions, an adiabatic efficiency...
AbstractGas-turbines are widely used to power aero planes because they are light, compact with a hig...
Calculations bawd on dynamometer test-stand data obtained on an 18-cylinder radial engine uxre made ...
An investigation was conducted to obtain fuel-consumption curves for a single-cylinder engine with a...
Calculations based on dynamometer test-stand data obtained on an 18-cylinder radial engine were made...
An analytical investigation was made of a topping cycle aircraft engine system which uses a cryogeni...
This report deals with the results of a test made upon a B. M. W. Engine in the altitude chamber of ...
DVL experimental and analytical work on the cooling of turbine blades by using ram air as the workin...
Small high-speed single-cylinder compression-ignition engines were tested to determine their perform...
Adjustable-stator turbines are applied to turbojet engines and probable performance is compared with...
Discussed here are the principles and operation of aircraft engine superchargers used to maintain an...
A parametric study was performed to determine the performance limits of a rotary combustion engine. ...
In part one of this report are presented the theoretical performance curves of an airplane engine eq...
This report contains the results of a test made upon a Maybach Engine in the altitude chamber of the...
In order to insure satisfactory turbine performance under five turbojet-engine operating conditions,...
The Rateau supercharger investigated had, under normal operating conditions, an adiabatic efficiency...
AbstractGas-turbines are widely used to power aero planes because they are light, compact with a hig...