Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Scott E. Meyer"'
Autor:
Neil S. Rodrigues, Oluwatobi Busari, YunTao Chen, Andrew J. North, Robert P. Lucht, William C.B. Senior, Colin T. McDonald, Scott E. Meyer, Walter Ray Laster
Publikováno v:
Combustion and Flame. 212:282-294
Advanced combustion technologies to limit NOX production are needed to meet rigorous emissions standards, which are required due to the harmful effect of NOX on the environment. One such advanced concept involves axially staging the fuel to create a
Autor:
Mark C. Grubelich, Dennis K. King, Scott E. Meyer, Sally P. M. Bane, James H. D'Entremont, Prashanth Bangalore Venkatesh
Publikováno v:
Journal of Petroleum Science and Engineering. 180:660-667
Large-scale extraction of oil and natural gas requires an effective method of generating a high surface area network of fractures, or the stimulation of existing fractures, in a formation in order to increase permeability. Conventional hydraulic frac
Publikováno v:
Journal of Propulsion and Power. 35:944-952
Nitrous oxide (N2O) has gained popularity as a unique oxidizer for propulsion applications due to its ability to decompose exothermically, producing nitrogen and oxygen. In the current work, the fl...
Autor:
Oluwatobi Busari, Colin T. McDonald, W. Ray Laster, Andrew J. North, Scott E. Meyer, Neil S. Rodrigues, Robert P. Lucht, William C.B. Senior, YunTao Chen
Publikováno v:
The Review of scientific instruments. 90(7)
The development and performance of a perforated plate burner (PPB) operating using premixed natural gas and air at engine-relevant inlet temperatures and combustor pressures with thermal powers up to 1 MW is discussed. A significant benefit of using
Autor:
Giuseppe Leccese, Francesco Battista, Vito Salvatore, Scott E. Meyer, Raffaele Votta, Francesco Nasuti, Marco Pizzarelli
Publikováno v:
Applied Thermal Engineering. 101:61-70
A test article has been specifically designed in order to investigate the methane behaviour inside rocket engine cooling channels. The test article is composed of a suitable copper-alloy block warmed up by cartridge heaters and of a single channel wi
Autor:
Scott E. Meyer, Valeria Andreoli, Jorge Saavedra, Ruth Herrero, David Lawrence, David Gonzalez Cuadrado, Terrence R. Meyer, J.P. Solano, Guillermo Paniagua
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 141
Following three decades of research in short duration facilities, Purdue University has developed an alternative turbine facility in view of the modern technology in computational fluid mechanics, structural analysis, manufacturing, heating, control,
Autor:
Marek Zreda, Roy M. Breckenridge, Bruce N. Bjornstad, David R. Gaylord, Gary A. Smith, Petteri Alho, Victor R. Baker, Mark R. Sweeney, Scott E. Meyer
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::17d79033992196fcd5e6b15d019f0096
http://juuli.fi/Record/0275002216
http://juuli.fi/Record/0275002216
Autor:
A. Gianvito, Vito Salvatore, S. Shark, A. Smoraldi, Raffaele Votta, Marco Pizzarelli, Francesco Nasuti, Giuseppe Leccese, Francesco Battista, R. Feddema, Scott E. Meyer
The use of the Methane as coolant in a regenerative liquid rocket engine (LRE) presents some difficulties since transcritical fluidynamics operating conditions occur in the cooling channels. Transcritical conditions cause large fluid properties varia
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c25e0060f4abef1beb559e641da39f56
http://hdl.handle.net/11573/626610
http://hdl.handle.net/11573/626610
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 134
An optically accessible combustion rig was constructed to study the combustion characteristics of a reactive jet in a vitiated crossflow. The rig features two staged combustion zones. The main combustion zone is a swirl stabilized dump combustor. The
Publikováno v:
Volume 2: Combustion, Fuels and Emissions, Parts A and B.
An optically accessible gas turbine combustor test rig was constructed to study the combustion characteristics of a coaxial hydrogen/air jet injected into a vitiated swirl crossflow. The test rig has two combustion zones. The main combustion zone (MC