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Gas turbine engines
Combustion chambers 27
Aircraft engines 21
Engine design 17
Computational fluid dynamics 12
Engine tests 11
Rotors 11
Flow distribution 9
Gas turbines 9
Gas-turbines 9
Mathematical models 9
Propulsion system performance 9
Ceramics 8
Engine control 8
Performance prediction 8
Compressors 7
Engine parts 7
Flow distortion 7
Fuel combustion 7
Laser induced fluorescence 7
Motors 7
Propulsion system configurations 7
Turbine blades 7
Automobile engines 6
Combustion 6
Cross flow 6
Fuel consumption 6
Heat resistant alloys 6
Heat transfer 6
High temperature 6

Probabilistic analysis of aircraft gas turbine disk life and reliability by Melis, Matthew E.

Workshop on Aerosols and Particulars from Aircraft Gas Turbine Engines

Wave-rotor-enhanced gas turbine engine demonstrator

Numerical study of stratified charge combustion in wave rotors / by Nalim, M. Razi

Development of a multiplane-multispeed balancing system for turbine engines by Martin, Michael R.

An integrated architecture for on-board aircraft engine performance trend monitoring and gas path fault diagnostics by Simon, Donald L.

Analysis of coupled seals, secondary and powerstream flow fields in aircraft and aerospace turbomachines by Athavale, M. M.

History of thermal barrier coatings for gas turbine engines emphasizing NASA's role from 1942 to 1990 / by Robert A. Miller

Optical and probe determination of soot concentrations in a model gas turbine combustor by Eckerle, Wayne Alan

Optimal tuner selection for Kalman filter-based aircraft engine performance estimation by Simon, Donald L.

Technology for Brayton-cycle space powerplants using solar and nuclear energy by English, Robert E. (Robert Eugene)

Integrated turbine tip clearance and gas turbine engine simulation / by Chapman, Jeffryes W.

Sensor and actuator needs for more intelligent gas turbine engines

Spreadsheet calculations for jets in crossflow opposed rows of inline and staggered holes and single and opposed rows with alternating hole sizes / by Holdeman, J. D.

Thermal and environmental barrier coating development for advanced propulsion engine systems by Zhu, Dongming

A data filter for identifying steady-state operating points in engine flight data for condition monitoring applications by Simon, Donald L.

High pressure regenerative turbine engine 21st century propulsion / by Lear, William E.

The high stability engine control (HISTEC) program : flight demonstration phase / by DeLaat, John C.

High Stability Engine Control (HISTEC) : flight demonstration results / by DeLaat, John C.

An N+3 technology level reference propulsion system / by Jones, Scott M., Haller, William J., Tong, Michael T.

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Probabilistic analysis of aircraft gas turbine disk life and reliability by Melis, Matthew E.

Workshop on Aerosols and Particulars from Aircraft Gas Turbine Engines

Wave-rotor-enhanced gas turbine engine demonstrator

Numerical study of stratified charge combustion in wave rotors / by Nalim, M. Razi

Development of a multiplane-multispeed balancing system for turbine engines by Martin, Michael R.

An integrated architecture for on-board aircraft engine performance trend monitoring and gas path fault diagnostics by Simon, Donald L.

Analysis of coupled seals, secondary and powerstream flow fields in aircraft and aerospace turbomachines by Athavale, M. M.

History of thermal barrier coatings for gas turbine engines emphasizing NASA's role from 1942 to 1990 / by Robert A. Miller

Optical and probe determination of soot concentrations in a model gas turbine combustor by Eckerle, Wayne Alan

Optimal tuner selection for Kalman filter-based aircraft engine performance estimation by Simon, Donald L.

Technology for Brayton-cycle space powerplants using solar and nuclear energy by English, Robert E. (Robert Eugene)

Integrated turbine tip clearance and gas turbine engine simulation / by Chapman, Jeffryes W.

Sensor and actuator needs for more intelligent gas turbine engines

Spreadsheet calculations for jets in crossflow opposed rows of inline and staggered holes and single and opposed rows with alternating hole sizes / by Holdeman, J. D.

Thermal and environmental barrier coating development for advanced propulsion engine systems by Zhu, Dongming

A data filter for identifying steady-state operating points in engine flight data for condition monitoring applications by Simon, Donald L.

High pressure regenerative turbine engine 21st century propulsion / by Lear, William E.

The high stability engine control (HISTEC) program : flight demonstration phase / by DeLaat, John C.

High Stability Engine Control (HISTEC) : flight demonstration results / by DeLaat, John C.

An N+3 technology level reference propulsion system / by Jones, Scott M., Haller, William J., Tong, Michael T.

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