Zobrazeno 1 - 10
of 16
pro vyhledávání: '"Robert C. Ryder"'
Publikováno v:
Journal of Natural Gas Chemistry. 18:145-155
Computational fluid dynamics modeling of the complex processes that occur within the burner of a gas turbine engine has become a critical step in the design process. However, due to computer limitations, it is very difficult to completely couple the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::82fc3dd4d28f450a168003a54d4373be
https://doi.org/10.1016/s1003-9953(08)60093-6
https://doi.org/10.1016/s1003-9953(08)60093-6
Autor:
Dale T. Shouse, William M. Roquemore, Robert C. Hendricks, Robert C. Ryder, J. R. Gallagher, J. A. Hendricks, Andreja Brankovic, David L. Burrus, N.-S. Liu, B. S. Duncan
Publikováno v:
International Journal of Rotating Machinery, Vol 7, Iss 6, Pp 375-385 (2001)
The Trapped Vortex Combustor (TVC) potentially offers numerous operational advantages over current production gas turbine engine combustors. These include lower weight, lower pollutant emissions, effective flame stabilization, high combustion efficie
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e54bde32673898d603fc89c49b65aaf3
https://doi.org/10.1155/s1023621x0100032x
https://doi.org/10.1155/s1023621x0100032x
Publikováno v:
SAE Technical Paper Series.
An approximation method for evaluation of the caloric equations used in combustion chemistry simulations is described. The method is applied to generate the equations of specific heat, static enthalpy, and Gibb's free energy for fuel mixtures of inte
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::25f4afe988c37ded2d2c4f3bfae4b994
https://doi.org/10.4271/2007-01-3790
https://doi.org/10.4271/2007-01-3790
Publikováno v:
44th AIAA Aerospace Sciences Meeting and Exhibit.
Time-dependent computational fluid dynamics (CFD) and combustion modeling is used to predict burning velocity of fuel-air mixtures in a closed vessel and swirlstabilized reacting flow in a representative turbine engine fuel nozzle. The purpose of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0a9c5cde86421beb411b25565640aa60
https://doi.org/10.2514/6.2006-806
https://doi.org/10.2514/6.2006-806
Autor:
Andy Brankovic, William M. Roquemore, Robert C. Ryder, Dale T. Shouse, Robert C. Hendricks, N.-S. Liu
Publikováno v:
43rd AIAA Aerospace Sciences Meeting and Exhibit.
An investigation is performed to evaluate the performance of a computational fluid dynamics (CFD) tool for the prediction of the reacting flow in a liquid-fueled combustor that uses water injection for control of pollutant emissions. The experiment c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::15b02cd1b53160b3580916bc5294b0d4
https://doi.org/10.2514/6.2005-215
https://doi.org/10.2514/6.2005-215
Publikováno v:
43rd AIAA Aerospace Sciences Meeting and Exhibit.
In this study a "smart" liquid fuel injector whose spray pattern can be modified by controlling the flow rates of two coaxial, counter swirling, oxidizer (air) streams that control the characteristics of the fuel spray was investigated under cold-flo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8a929f35d45a55a20e779196c39a2301
https://doi.org/10.2514/6.2005-213
https://doi.org/10.2514/6.2005-213
Publikováno v:
SAE Technical Paper Series.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1a170121df9ef16022d30d66e531ddb8
https://doi.org/10.4271/2004-01-3557
https://doi.org/10.4271/2004-01-3557
Publikováno v:
42nd AIAA Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ab43a72acd00a1975eb79e2d5b803d10
https://doi.org/10.2514/6.2004-328
https://doi.org/10.2514/6.2004-328
Autor:
William M. Roquemore, Robert C. Hendricks, Andreja Brankovic, Robert C. Ryder, N.-S. Liu, Dale T. Shouse
Publikováno v:
Volume 1: Turbo Expo 2004.
Numerical simulations are performed to predict the flow properties in a liquid spray droplets fueled Trapped Vortex Combustor (TVC) sector rig. The quantities studied include aerodynamics, pressure drop, spray droplets trajectories, evaporation, mixi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::76f3e69316b82375a704c859d0cb9793
https://doi.org/10.1115/gt2004-53225
https://doi.org/10.1115/gt2004-53225
Autor:
J. A. Hendricks, Dale T. Shouse, Robert C. Ryder, N.-S. Liu, William M. Roquemore, Robert C. Hendricks, Andreja Brankovic, J. R. Gallagher, Clayton Stuart Cooper, David L. Burrus
Publikováno v:
ICIASF 2001 Record, 19th International Congress on Instrumentation in Aerospace Simulation Facilities (Cat. No.01CH37215).
This paper described an experimental and computational effort aimed at understanding diffuser exit profiles, for a lobed duct design that will potentially be used for higher Mach combustion evaluations in the Trapped Vortex Combustor (TVC). Experimen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::56cedc58fd460585120bbe03307ed712
https://doi.org/10.1109/iciasf.2001.960278
https://doi.org/10.1109/iciasf.2001.960278