Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Craig Neuroth"'
Publikováno v:
Volume 4A: Combustion, Fuels, and Emissions.
The capability of current turbomachinery-based engines limit the obtainable altitude and flight Mach number of modern aircraft. Maturing hypersonic technologies such as ram and scramjets allow greatly increased flight velocity but are not able to pow
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b6aa728c9710f3cce2352d5437e4125b
https://doi.org/10.1115/gt2018-75570
https://doi.org/10.1115/gt2018-75570
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c357c74a16b989d40da3c9f43cf5b92d
https://doi.org/10.2514/6.2016-0450
https://doi.org/10.2514/6.2016-0450
Autor:
Justin T. Gross, David L. Burrus, Andrew W. Caswell, Craig Neuroth, Dale T. Shouse, Timothy J. Erdmann
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Volatile fuel costs have initiated a global sprint for technologies that will increase fuel efficiency in gas turbine engines, which continue to be a primary propulsion system for commercial and military aircraft. The Ultra-Compact Combustor (UCC) is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4f45b076deefc1da6676dcc7dfb68f2c
https://doi.org/10.2514/6.2016-0446
https://doi.org/10.2514/6.2016-0446
Autor:
Dale T. Shouse, J. S. Stutrud, Edwin Corporan, Amy Lynch, Craig Neuroth, Charles W. Frayne, Robert C. Hendricks, Capt. T. Hankins
Publikováno v:
ISRN Mechanical Engineering. 2012:1-26
Alternate aviation fuels for military or commercial use are required to satisfy MIL-DTL-83133F or ASTM D 7566 standards, respectively, and are classified as “drop-in’’ fuel replacements. To satisfy legacy issues, blends to 50% alternate fuel wi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::426e67c0e40b486aaebdc45bbcb02c0e
https://doi.org/10.5402/2012/684981
https://doi.org/10.5402/2012/684981
Autor:
Laura A. Kranendonk, Dale T. Shouse, Craig Neuroth, Andrew W. Caswell, Scott T. Sanders, James R. Gord, Christopher L. Hagen
Publikováno v:
Journal of Propulsion and Power. 25:859-863
Gas-temperature measurements in the combustion zone of a high-pressure gas-turbine-combustor sector rig were made with a Fourier-domain mode-locked laser using wavelength-agile absorption-spectroscopy techniques. These measurements are among the firs
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3cc0ee977ccf6091eac800475c9ff1f3
https://doi.org/10.2514/1.41587
https://doi.org/10.2514/1.41587
Autor:
David L. Blunck, Justin T. Gross, Andrew W. Caswell, Amy Lynch, Craig Neuroth, Timothy J. Erdmann, Alejandro M. Briones, David L. Burrus, Dale T. Shouse, Balu Sekar
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Significant benefits can be obtained with respect to engine thrust-to-weight ratio and specific fuel consumption if the length, weight, and pressure drop of the combustor can be reduced. The ultra-compact combustor (UCC) has the potential to aid the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4cec45a0551a3c4d14518c3d12280cab
https://doi.org/10.2514/6.2014-3630
https://doi.org/10.2514/6.2014-3630
Autor:
Daniel R. Richardson, Andrew W. Caswell, Amy Lynch, Craig Neuroth, David L. Blunck, Dale T. Shouse, Joseph Zelina, David L. Burrus, Timothy J. Erdmann
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 136
Reducing the weight and decreasing pressure losses of aviation gas turbine engines improves the thrust-to-weight ratio and improves efficiency. In ultra-compact combustors (UCC), engine length is reduced and pressure losses are decreased by merging a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7b79d59fbee8a3e4ec36f4f3f559d75a
https://doi.org/10.1115/1.4026975
https://doi.org/10.1115/1.4026975
Publikováno v:
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
A novel Ultra-Compact Combustor (UCC) that operates as a main combustor in a gas turbine engine is modeled with the Trapped Vortex Combustor (TVC) incorporating three inlet guide vanes (IGVs), containing no radial vane cavities (RVC), and three deswi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ebad493c73b09989f792c070ee25b8c6
https://doi.org/10.2514/6.2013-1045
https://doi.org/10.2514/6.2013-1045
Publikováno v:
28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference.
Optical measurement techniques are required to determine flow-field parameters for the development and evaluation of advanced combustion systems. Parameters include but are not limited to velocity, temperature, and species concentrations. There are m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aef8ddf050b42a2d0248743c20f42086
https://doi.org/10.2514/6.2012-2884
https://doi.org/10.2514/6.2012-2884
Autor:
J. S. Stutrud, Terry Hankins, Dale T. Shouse, Charles W. Frayne, Robert C. Hendricks, Anna E. Thomas, Nikita T. Saxena, Edwin Corporan, Amy Lynch, Craig Neuroth
Publikováno v:
ISRN Mechanical Engineering.
In order to realize alternative fueling for military and commercial use, industry guidelines be met. These aviation fueling requirements are outlined in MIL-DTL-83133F(2008) or ASTM D 7566-Annex standards and are classified as “drop-in” fuel repl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9b2301db67d925e32c1750a22cb4fc1c