A high pressure, high temperature combustor and turbine-cooling test facility [PDF]
A new test facility is being constructed for developing turbine-cooling and combustor technology for future generation aircraft gas turbine engines. Prototype engine hardware will be investigated in this new facility at gas stream conditions up to 2480 K
Cochran, R. P., Norris, J. W.
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The Effect of Physical Faults on a Three-Shaft Gas Turbine Performance at Full- and Part-Load Operation. [PDF]
Sensors (Basel), 2022 Salilew WM +4 more
europepmc +1 more source
Selection of natural Gas Fired Advanced Turbine Systems (GFATS) program - Task 3. Topical report
, 1994 Allison Engine Co., Indianapolis, IN (United States)
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Digital Control of the WR21 Intercooled Recuperated Gas Turbine [PDF]
, 1995 R. J. Carlson, R. E. Olson
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Non-Invasive Acoustic Monitoring of Gas Turbine Units by Fiber Optic Sensors. [PDF]
Sensors (Basel), 2022 Stepanov KV +5 more
europepmc +1 more source
A Critical Appraisal of Some Current Incidence Loss Models for the Stator and Rotor of a Mixed Flow Gas Turbine [PDF]
, 1982 F. Fairbanks
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Laser-optical blade tip clearance measurement system [PDF]
A laser-optical measurement system was developed to measure single blade tip clearances and average blade tip clearances between a rotor and its gas path seal in rotating component rigs and complete engines.
Barranger, J. P., Ford, M. J.
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Investigation of Combustion of the Gas Turbine Engine from Kerosene and Biokerosene and Their Soot Characteristics in Diffusion Flames. [PDF]
ACS Omega, 2022 Hong TD +3 more
europepmc +1 more source
CFD Modeling of Hydrogen Combustion for Gas Turbine Applications
, 2022 Peter Strakey
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