Zobrazeno 1 - 10 of 15 pro vyhledávání: '"Carl A. Trexler"'
1
Mach 4 Performance of Hypersonic Inlet with Rectangular-to-Elliptical Shape Transition
Autor: Carl A. Trexler, Michael K. Smart
Publikováno v: Journal of Propulsion and Power. 20:288-293
Wind-tunnel testing of a hypersonic inlet with rectangular-to-elliptical shape transition has been conducted at Mach 4.0. This fixed geometry inlet had a geometric contraction ratio of 4.8 and was designed using a quasi-streamline tracing technique t
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::d6afb146ebd098378ad61ea1271c5a3e
https://doi.org/10.2514/1.1296
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2
Unsteady pressure behavior in a ramjet/scramjet inlet
Autor: Saied Emami, Patrick E. Rodi, Carl A. Trexler
Publikováno v: Journal of Propulsion and Power. 12:486-493
Mean and time-accurate pressures have been measured in the inlet of a dual-mode, ramjet/scramjet configuration. This configuration was designed for low hypersonic Mach number operation using a hydrocarbon-based fuel. The time-accurate measurements ar
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::aa73a94db0aebc5a93cad5f4b1acebf1
https://doi.org/10.2514/3.24061
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3
Three-dimensional simulation of a translating strut inlet
Autor: Carl A. Trexler, Julie A. Hudgens, D. J. Singh
Publikováno v: Journal of Propulsion and Power. 10:191-197
A three-dimensional Navier-Stokes code is used to numerically simulate the flow through a translating strut scramjet inlet. The inlet has variable geometry for efficient operation over a wide speed range. Overall flow-field features such as the corne
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0e49a1923ac2711c4fd21a978dfb3ed9
https://doi.org/10.2514/3.23729
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4
Numerical study of the effects of reverse sweep on scramjet inlet performance
Autor: Ajay Kumar, D. J. Singh, Carl A. Trexler
Publikováno v: Journal of Propulsion and Power. 8:714-719
A comparative numerical study of performance parameters of a similar and an opposite sweep sidewall compression inlet is made. The focus of the study is the investigation of the impact of alternate backward-forward sweep on the compression sidewalls
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::59a2623d3a283b8f9bd71f3d2c307deb
https://doi.org/10.2514/3.23537
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7
Mach 4 Performance of a Fixed-Geometry Hypersonic Inlet with Rectangular-to-Elliptical Shape Transition
Autor: Carl A. Trexler, Michael K. Smart
Publikováno v: 41st Aerospace Sciences Meeting and Exhibit.
Wind-tunnel testing of a hypersonic inlet with rectangular-to-elliptical shape transition has been conducted at Mach 4.0. These tests were performed to investigate the starting and back-pressure limits of this fixed-geometry inlet at conditions well
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::dd8ad7831f9956d6bdd3692c7d4e9272
https://doi.org/10.2514/6.2003-12
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8
A combined experimental/computational investigation of a rocket based combined cycle inlet
Autor: Carl A. Trexler, Michael K. Smart, Allen L. Goldman
Publikováno v: 39th Aerospace Sciences Meeting and Exhibit.
A rocket based combined cycle inlet geometry has undergone wind tunnel testing and computational analysis with Mach 4 flow at the inlet face. Performance parameters obtained from the wind tunnel tests were the mass capture, the maximum back-pressure,
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::f9d781d3ab9dc0af5c358410cefaa386
https://doi.org/10.2514/6.2001-671
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