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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
