Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Wendy S. Barankiewicz"'
Publikováno v:
Journal of Aircraft. 33:457-462
In this article NPARC calculations of the F/A-18A High Alpha Research Vehicle installed inlet flow are compared with flight test at a Mach number of 0.3, angles of attack of 30 and 60 deg, and nonzero sideslip angle. Predicted forebody, leading-edge
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::09155a19845236b00d606dfcc66df24a
https://doi.org/10.2514/3.46966
https://doi.org/10.2514/3.46966
Publikováno v:
Journal of Aircraft. 33:463-469
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c815e105d87125738f57c08026846341
https://doi.org/10.2514/3.46967
https://doi.org/10.2514/3.46967
Publikováno v:
Journal of Propulsion and Power. 10:198-203
Full-scale ejector experiments are expensive and difficult to implement at engine exhaust temperatures. For this reason the utility of using similarity principles, in particular the Munk and Prim principle for isentropic flow, was explored. Static pe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e0c939525d6c1d0bc04109910d0fb9b5
https://doi.org/10.2514/3.23730
https://doi.org/10.2514/3.23730
Publikováno v:
Volume 1: Turbomachinery.
The impact of hub leakage flow associated with the clearance gaps of hub-shrouded variable-geometry stator rows in axial compressors is investigated experimentally. The objectives of this work are to investigate the sensitivity of performance to chor
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::29bb579723e4404b75712f722e7772d0
https://doi.org/10.1115/98-gt-194
https://doi.org/10.1115/98-gt-194
Publikováno v:
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery.
The results of an experimental investigation to determine the impact of stator row indexing or clocking on multistage axial compressor performance are presented. Testing was conducted in the NASA Lewis Research Center’s Four-Stage Axial Compressor
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a961f73775497ac04326e37b01f4beaf
https://doi.org/10.1115/97-gt-496
https://doi.org/10.1115/97-gt-496
Publikováno v:
31st Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8bcd130274a6d7da4219e56ac8f61e10
https://doi.org/10.2514/6.1995-2758
https://doi.org/10.2514/6.1995-2758
Publikováno v:
28th Joint Propulsion Conference and Exhibit.
Full temperature ejector model simulations are expensive, and difficult to implement experimentally. If an approximate similarity principle could be established, properly chosen performance parameters should be similar for both hot and cold flow test
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3a4193d45c57252d57b23243c1ef91ff
https://doi.org/10.2514/6.1992-3792
https://doi.org/10.2514/6.1992-3792
Autor:
Wendy S. Barankiewicz
Publikováno v:
27th Joint Propulsion Conference.
The design and development of thrust augmenting STOVL ejectors has typically been based on experimental iteration (i.e., trial and error). Static performance tests of a full scale vertical lift ejector were performed at primary flow temperatures up t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c50d22d945bfae05da21fb41eeb782cd
https://doi.org/10.2514/6.1991-1902
https://doi.org/10.2514/6.1991-1902
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