Add to ORKGA computerized method which utilizes the engine performance data is described. The method estimates the installed performance of aircraft gas turbine engines. This installation includes: engine weight and dimensions, inlet and nozzle internal performance and drag, inlet and nacelle weight, and nacelle drag
In support of the Fundamental Aeronautics Program, Subsonic Rotary Wing Project, further gas turbine...
An open cycle gas turbine numerical modelling code suitable for thermodynamic performance analysis (...
The cost and risk associated with the design and operation of gas turbine engine systems has led to ...
A computerized method which utilizes the engine performance data and estimates the installed perform...
A computerized method which utilizes the engine performance data and estimates the installed perform...
A simplified method is presented for computing the installation losses of aircraft gas turbine propu...
The computational techniques utilized to determine the optimum propulsion systems for future aircraf...
Weight and envelope dimensions of aircraft gas turbine engines are estimated within plus or minus 5%...
A computer code capable of simulating almost any conceivable turbine engine is described. This code ...
As part of the NASA-sponsored Engine Component Improvement (ECI) Program, a feasibility analysis of ...
A computerized method was developed to estimate weight and envelope dimensions of large and small ga...
In order to understand the operation and the interaction of jet-engine components during engine oper...
The methods which have been used by the NASA Lewis Research Center for predicting Brayton Cycle comp...
Program uses component performance maps to enable user to do analytical engine cycle calculations. E...
The use of computerized simulations of the steady state and transient performance of jet engines thr...
In support of the Fundamental Aeronautics Program, Subsonic Rotary Wing Project, further gas turbine...
An open cycle gas turbine numerical modelling code suitable for thermodynamic performance analysis (...
The cost and risk associated with the design and operation of gas turbine engine systems has led to ...
A computerized method which utilizes the engine performance data and estimates the installed perform...
A computerized method which utilizes the engine performance data and estimates the installed perform...
A simplified method is presented for computing the installation losses of aircraft gas turbine propu...
The computational techniques utilized to determine the optimum propulsion systems for future aircraf...
Weight and envelope dimensions of aircraft gas turbine engines are estimated within plus or minus 5%...
A computer code capable of simulating almost any conceivable turbine engine is described. This code ...
As part of the NASA-sponsored Engine Component Improvement (ECI) Program, a feasibility analysis of ...
A computerized method was developed to estimate weight and envelope dimensions of large and small ga...
In order to understand the operation and the interaction of jet-engine components during engine oper...
The methods which have been used by the NASA Lewis Research Center for predicting Brayton Cycle comp...
Program uses component performance maps to enable user to do analytical engine cycle calculations. E...
The use of computerized simulations of the steady state and transient performance of jet engines thr...
In support of the Fundamental Aeronautics Program, Subsonic Rotary Wing Project, further gas turbine...
An open cycle gas turbine numerical modelling code suitable for thermodynamic performance analysis (...
The cost and risk associated with the design and operation of gas turbine engine systems has led to ...