Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Ashlie B. Flegel"'
Autor:
Ashlie B. Flegel
Publikováno v:
Journal of Turbomachinery. 143
A Honeywell Uncertified Research Engine was exposed to various ice crystal conditions in the NASA Glenn Propulsion Systems Laboratory. Simulations using NASA’s 1D Icing Risk Analysis tool were used to determine potential inlet conditions that could
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cf64f93df7a0ce091d8ba4225ad2f7fb
https://doi.org/10.1115/1.4050669
https://doi.org/10.1115/1.4050669
Publikováno v:
SAE Technical Paper Series.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a3b9d8ec4a1439649036cd0115e866d4
https://doi.org/10.4271/2019-01-1965
https://doi.org/10.4271/2019-01-1965
Autor:
Ashlie B. Flegel
Publikováno v:
9th AIAA Atmospheric and Space Environments Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c6be54a12c6115339eb4dac4bad03af3
https://doi.org/10.2514/6.2017-4085
https://doi.org/10.2514/6.2017-4085
Autor:
Ashlie B. Flegel, Michael J. Oliver
Publikováno v:
8th AIAA Atmospheric and Space Environments Conference.
Preliminary results from the heavily instrumented ALF502R-5 engine test conducted in the NASA Glenn Research Center Propulsion Systems Laboratory are discussed. The effects of ice crystal icing on a full scale engine is examined and documented. This
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::58faaad004c5b1b253684218c2843b80
https://doi.org/10.2514/6.2016-3894
https://doi.org/10.2514/6.2016-3894
Autor:
David T. Booth, Ashlie B. Flegel
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
A computational assessment of the aerodynamic performance of the midspan section of a variable-speed power-turbine blade is described. The computation comprises a periodic single blade that represents the 2-D Midspan section VSPT blade that was teste
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::049a4b1361bb6ff45a7c3ae0686b0f61
https://doi.org/10.2514/6.2015-3928
https://doi.org/10.2514/6.2015-3928
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
The effects of high inlet turbulence intensity on the aerodynamic performance of a variable speed power turbine blade are examined over large incidence and Reynolds number ranges. These results are compared to previous measurements made in a low turb
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a1a4735ace7b13d40fa45fcf9fd2a6f5
https://doi.org/10.2514/6.2014-3933
https://doi.org/10.2514/6.2014-3933
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Constant temperature hotwire anemometry data were acquired to determine the inlet turbulence conditions of a transonic turbine blade linear cascade. Flow conditions and angles were investigated that corresponded to the take-off and cruise conditions
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4bc93f2e971c693e8d94f73fe2d79ff1
https://doi.org/10.2514/6.2014-3934
https://doi.org/10.2514/6.2014-3934
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Variable-Speed Power Turbines (VSPT) for rotorcraft applications operate at low Reynolds number and over a wide range in incidence associated with shaft speed change. A comprehensive linear cascade data set obtained includes the effects of Reynolds n
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::395d9e0deaf031fc40f79b1962b9bbf3
https://doi.org/10.2514/6.2014-3935
https://doi.org/10.2514/6.2014-3935