Results 111 to 120 of about 10,932 (224)

Laser-optical blade tip clearance measurement system [PDF]

open access: yes
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.
core   +1 more source

Flow studies in a wet steam turbine [PDF]

open access: yes
The design and test results of a four stage wet vapor turbine operating with slightly superheated inlet steam and expanding to 10% exit moisture are presented.
Evans, D. H., Pouchot, W. D.
core   +1 more source

Thermal stress analysis of a new turbine shroud seal concept [PDF]

open access: yes
The thermal stress field of a two piece turbine shroud seal concept was analyzed and results compared to one piece designs by finite element analysis.
Handschuh, R. F.
core   +1 more source

Revised FORTRAN program for calculating velocities and streamlines on the hub-shroud midchannel stream surface of an axial-, radial-, or mixed-flow turbomachine or annular duct. 1: User's manual [PDF]

open access: yes
A FORTRAN 4 computer program was developed that obtains a detailed subsonic or shock-free transonic flow solution on the hub-shroud midchannel stream surface of a turbomachine.
Katsanis, T., Mcnally, W. D.
core   +1 more source

Gas-path seal technology [PDF]

open access: yes
Improved gas-path seals are needed for better fuel economy, longer performance retention, and lower maintenance, particularly in advanced, high-performance gas turbine engines.
Zuk, J.
core   +1 more source

Numerical calculation of the internal flow field in a centrifugal compressor impeller [PDF]

open access: yes
An iterative numerical method has been developed for the calculation of steady, three-dimensional, viscous, compressible flow fields in centrifugal compressor impellers.
Harp, J. L., Jr., Liu, C. Y., Walitt, L.
core   +1 more source

Home - About - Disclaimer - Privacy