Zobrazeno 1 - 10 of 12 pro vyhledávání: '"Dennis C. Berridge"'
1
Boundary Layer Transition Preflight Experiments in a Mach-6 Quiet Tunnel
Autor: Steven P. Schneider, Brandon C. Chynoweth, Gregory McKiernan, Dennis C. Berridge, Bradley M. Wheaton
Publikováno v: Journal of Spacecraft and Rockets. 58:54-66
Experiments on a subscale model of the U.S. Air Force Office of Scientific Research Boundary Layer Transition flight experiment were made in the Boeing/Air Force Office of Scientific Research Mach-...
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::10bfc838b51d1fe6e144637121ef8b0e
https://doi.org/10.2514/1.a34772
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6
Boundary-Layer Transition Experiments in a Hypersonic Quiet Wind Tunnel
Autor: Steven P. Schneider, Dennis C. Berridge, Christopher Ward, Andrew D. Abney, Roger Greenwood
Publikováno v: 43rd Fluid Dynamics Conference.
This paper reports the progress of three projects in the Boeing/AFOSR Mach-6 quiet tunnel at Purdue University. The first project used a 7-deg half-angle cone at 6-deg angleof-attack with temperature-sensitive paint applied to the frustum and small r
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::b420c96785ac09e4cb84cb9a362bd16b
https://doi.org/10.2514/6.2013-2738
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7
Pressure Fluctuation Measurements in the NASA Langley 20-Inch Mach 6 Wind Tunnel
Autor: Shann J. Rufer, Dennis C. Berridge
Publikováno v: 42nd AIAA Fluid Dynamics Conference and Exhibit.
Experiments have been carried out in the NASA Langley Research Center 20-Inch Mach 6 Wind Tunnel to measure the freestream pressure fluctuations, or tunnel noise, using a pitot rake. These experiments are part of an on-going effort to characterize th
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::c02e07e1473942e9a0912e8d36d96ccf
https://doi.org/10.2514/6.2012-3262
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8
Hypersonic Boundary-Layer Transition Experiments in the Boeing/AFOSR Mach-6 Quiet Tunnel
Autor: Ryan P. K. Luersen, Amanda Chou, Laura E Letterman, Christopher Ward, Brad Wheaton, Dennis C. Berridge, Steven P. Schneider
Publikováno v: 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
This paper reports progress from six different projects studying hypersonic boundarylayer transition. Efforts to measure instabilities in the wake of an isolated roughness element in the laminar nozzle-wall boundary layer of the BAM6QT are on-going.
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::ff6e7fa454b5299c1f4feebd2f6bc185
https://doi.org/10.2514/6.2012-282
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9
Experimental Study of Second-Mode Instabilities on a 7-Degree Cone at Mach 6
Autor: Shann J. Rufer, Dennis C. Berridge
Publikováno v: 41st AIAA Fluid Dynamics Conference and Exhibit.
Experiments have been carried out in the NASA Langley Research Center 20-Inch Mach 6 Air Tunnel to measure the second-mode boundary-layer instability on a 7° half-angle cone using high-frequency pressure sensors. Data were obtained with both blunt a
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::27419350fa97e5f325d57afe82b0a7f5
https://doi.org/10.2514/6.2011-3877
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