Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Scott R. Thomas"'
Autor:
Scott R. Thomas
Publikováno v:
Pace Law Review. 39:875
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::00d40a80493562d79ffab2469ffa13a2
https://doi.org/10.58948/2331-3528.2004
https://doi.org/10.58948/2331-3528.2004
Publikováno v:
27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference.
The Hypersonic Tunnel Facility (HTF) located at the NASA Glenn Research Center s Plum Brook Station in Sandusky, Ohio, is the nation s only large-scale, non-vitiated, hypersonic propulsion test facility. The HTF, with its 4-story graphite induction h
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4e68cfdf5cbdf4cb8324ce2b1cfe3f74
https://doi.org/10.2514/6.2010-4533
https://doi.org/10.2514/6.2010-4533
Publikováno v:
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference.
The propulsion research portfolio of the National Aeronautics and Space Administration Fundamental Aeronautics Program Hypersonics Project encompasses a significant number of technical tasks that are aligned to achieve mastery and intellectual stewar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3bfa669f2d51af67e6b36dea88f219ab
https://doi.org/10.2514/6.2009-7277
https://doi.org/10.2514/6.2009-7277
Publikováno v:
Journal of Propulsion and Power. 14:1065-1067
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fd4d7aa4bd473eff8504c7388be66ecb
https://doi.org/10.2514/2.5375
https://doi.org/10.2514/2.5375
Autor:
James E. Fittje, Richard S. Dyer, Dean P. Petters, H. Douglas Perkins, Daniel E. Paxson, Louis A. Povinelli, Scott R. Thomas
Publikováno v:
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
A number of Pulse Detonation Engine (PDE) performance modeling methodologies have been advanced over the last 15 years, varying widely in approach. In an effort to evaluate the effectiveness of several of these approaches, two data points from a sing
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d23550de742c5c240cdd5efed1eb55f7
https://doi.org/10.2514/6.2005-3831
https://doi.org/10.2514/6.2005-3831
Publikováno v:
41st Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9eac449e37ebae6c57cc96b19844e8f7
https://doi.org/10.2514/6.2003-16
https://doi.org/10.2514/6.2003-16
Publikováno v:
International Aerospace Planes and Hypersonics Technologies.
The NASA Lewis Research Center's Hypersonic Tunnel Facility (HTF) is a free-jet, blowdown propulsion test facility that can simulate up to Mach-7 flight conditions with true air composition. Mach-5, -6, and -7 nozzles, each with a 42 inch exit diamet
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::04976e4acb38c272d6b4ee141c1a2c6b
https://doi.org/10.2514/6.1995-6146
https://doi.org/10.2514/6.1995-6146
Autor:
Scott R. Thomas, Beverly Duncan
Publikováno v:
28th Joint Propulsion Conference and Exhibit.
A computational analysis of a ramjet engine at Mach 3.5 has been conducted and compared to results obtained experimentally. This study focuses on the behavior of the inlet both with and without combustor backpressure. Increased backpressure results i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8de43d4369726fa48ff5319921f15de7
https://doi.org/10.2514/6.1992-3102
https://doi.org/10.2514/6.1992-3102
Autor:
Scott R. Thomas, R. Wayne Guy
Publikováno v:
16th Aerodynamic Ground Testing Conference.
Consideration is given to the development of testing methods for the National Aerospace Plane (NASP) program, focusing on techniques for simulating and testing scramjet engines and scramjet engine components during flight from Mach 4 to Mach 20. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a48e654d1a2c7c5e2e4e08b8cd4eec3c
https://doi.org/10.2514/6.1990-1388
https://doi.org/10.2514/6.1990-1388
Publikováno v:
23rd Joint Propulsion Conference.
The test flow at the exits of two square cross-section contoured nozzles with nominal exit Mach numbers of 4.7 and 6 has been studied as calibration data for the NASA-Langley Arc-Heated Scramjet Test Facility over simulated flight conditions from Mac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3a29f7b4db999ef70e6eab3219848974
https://doi.org/10.2514/6.1987-2165
https://doi.org/10.2514/6.1987-2165