Zobrazeno 1 - 6
of 6
pro vyhledávání: '"C. T. Norgren"'
Autor:
D. S. Goldin, C. T. Norgren
Publikováno v:
AIAA Journal. 3:1943-1945
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9556299160f8927f379a526f11b9f33a
https://doi.org/10.2514/3.3285
https://doi.org/10.2514/3.3285
Autor:
C. T. Norgren, S. M. Riddlebaugh
Publikováno v:
21st Aerospace Sciences Meeting.
A reverse flow combustor liner constructed of Lamilloy (a multilaminate transpiration type material) is compared both analytically and experimentally with a conventional splash film-cooled design with the same combustor configuration. Comparison of s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::81433fb9b33e28f74c7346cd549f5b2b
https://doi.org/10.2514/6.1983-337
https://doi.org/10.2514/6.1983-337
Publikováno v:
22nd Aerospace Sciences Meeting.
Advanced commercial and military gas turbine engines may operate at combustor outlet temperatures in excess of 1920 K (3000 F). At these temperatures combustors liners experience extreme convective and radiative heat fluxes. The ability of a plasma s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0a214108a9277fb32e24dd7bad9eb484
https://doi.org/10.2514/6.1984-363
https://doi.org/10.2514/6.1984-363
Autor:
S. M. Riddlebaugh, C. T. Norgren
Publikováno v:
21st Aerospace Sciences Meeting.
The effect of fuel type on the performance of various fuel injectors was investigated in a reverse flow combustor. Combustor performance and emissions are documented for simplex pressure atomizing, spill flow, and airblast fuel injectors using a broa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d3799feb25590530a1ba093be95f0718
https://doi.org/10.2514/6.1983-154
https://doi.org/10.2514/6.1983-154
Autor:
C. T. Norgren, S. M. Riddlebaugh
Publikováno v:
17th Joint Propulsion Conference.
As part of a continuing effort at the Lewis Research Center to improve performance, emissions, and reliability of turbine machinery, an investigation of fuel injection technique and effect of fuel type on small gas turbine combustors was undertaken.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::06f53829df0d76a5c9f0d90a421724e0
https://doi.org/10.2514/6.1981-1388
https://doi.org/10.2514/6.1981-1388
Autor:
C. T. Norgren, S. M. Riddlebaugh
Publikováno v:
21st Joint Propulsion Conference.
Component research for advanced small gas turbine engines is currently underway at the NASA Lewis Research Center. As part of this program, a basic reverse-flow combustor geometry was being maintained while different advanced liner wall cooling techn
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ba0e48ea8e7ddaf841ab2a338a3490a6
https://doi.org/10.2514/6.1985-1290
https://doi.org/10.2514/6.1985-1290