Zobrazeno 1 - 10 of 16 pro vyhledávání: '"Jason M. Merret"'
1
Impact of Liquid-Hydrogen Fuel-Cell Electric Propulsion on Aircraft Configuration and Integration
Autor: Elias G. Waddington, Jason M. Merret, Phillip J. Ansell
Publikováno v: Journal of Aircraft. :1-13
This study considers the aircraft configuration impacts of a liquid-hydrogen fuel-cell electric propulsion system when integrated into a single-aisle, transport-class aircraft having comparable performance capability of a Boeing 737-800. This study d
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::6fc337ebfb74d697f54c5667058cd328
https://doi.org/10.2514/1.c037237
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6
Real-time dynamic 3D view for tactical weather avoidance using head tracking
Autor: Jason M. Merret, Christopher Nusbaum, Daniela Kratchounova, Albert Helfrick, James G. Ladesic
Publikováno v: 2017 IEEE/AIAA 36th Digital Avionics Systems Conference (DASC).
Today, some of the more advanced flight decks are equipped with both a lateral and vertical presentation of weather products (e.g. ownship RADAR) on a multi-function display (MFD). The lateral view is overlaid on a map display, whereas the vertical v
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::e06fa54a2f79c35d7b3e0b5509fb6b49
https://doi.org/10.1109/dasc.2017.8102061
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7
Force and Moment Test on a Low Boom Configuration in Glenn's 8 x 6 Wind Tunnel (Invited)
Autor: George R. Hicks, Jason M. Merret, Thomas R. Wayman
Publikováno v: 29th AIAA Applied Aerodynamics Conference.
Experimental aerodynamic data are presented for a wind tunnel model of a low-boom aircraft concept conducted in the NASA Glenn Research Center 8- by 6-foot Supersonic Wind Tunnel. This aircraft concept, originally designed for experimental investigat
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::139703d78723933bd7bc239d16b5ca01
https://doi.org/10.2514/6.2011-3332
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9
CFD Results for an Axisymmetric Isentropic Relaxed Compression Inlet
Autor: Kathleen M. Tacina, Timothy R. Conners, Jason M. Merret, Stefanie M. Hirt, Donald C. Howe
Publikováno v: 46th AIAA Aerospace Sciences Meeting and Exhibit.
The OVERFLOW code was used to calculate the flow field for a family of five relaxed compression inlets, which were part of a screening study to determine a configuration most suited to the application of microscale flow control technology as a replac
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::2886e1eb80fe21e4c14b478d58320619
https://doi.org/10.2514/6.2008-92
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10
Wind Tunnel Testing of an Axisymmetric Isentropic Relaxed External Compression Inlet at Mach 1.97 Design Speed
Autor: Timothy R. Conners, Jason M. Merret, Kathleen M. Tacina, Donald C. Howe, Stefanie M. Hirt
Publikováno v: 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
An alternative inlet design method employing isentropic relaxed compression has been developed by Gulfstream Aerospace Corporation for improving net propulsion system performance and reducing sonic boom strength. To substantiate results from prior an
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::bc3afc6cbdecaaea6a78998bb156bdea
https://doi.org/10.2514/6.2007-5066
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