Jet engines

Results: 1048



#Item
181Synthetic fuels / Jet engines / Energy conversion / Chemical engineering / Gasification / Coal gas / Combustor / Mathematical optimization / Syngas / Energy / Fuel gas / Technology

Annual Research Report 2006

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Source URL: criepi.denken.or.jp

Language: English - Date: 2008-09-29 03:41:19
182Jet engines / Propelling nozzle / Inkjet printer / Technology / Matter / Business / Spray nozzle / Fluid mechanics / Nozzles / Spray

PRODUCT tech note Dead Sure®/TeeJet DRS For reduction of driftable fines. Dead Sure DRT is both a spray drift risk reducing adjuvant for fallow herbicides and an adjuvant to improve the efficacy of the fallow herbicides

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Source URL: www.caltex.com.au

Language: English - Date: 2014-01-08 18:09:15
183Aerospace engineering / Aeronautics / Jet engines / De-ice / Japan Aerospace Exploration Agency / Wake turbulence / Icing conditions / Bleed air / Flight test / Aviation / Transport / Air safety

JAXA Aeronautics Magazine Flight Path No.3/4

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Source URL: www.aero.jaxa.jp

Language: English - Date: 2014-12-11 05:14:45
184Mechanical engineering / Aerodynamics / Turbines / Compressors / Gas turbine / Marine propulsion / Genetic algorithm / Combustor / Jet engines / Fluid dynamics / Fluid mechanics

Principal Research Results Optimal Rotation Planning Method for Gas Turbine Hot Gas Path Parts Background Gas turbine hot gas path parts, e.g. blades, vanes, and combustors, are used in severe high temperature condition

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Source URL: criepi.denken.or.jp

Language: English - Date: 2008-09-29 03:15:22
185Japanese space program / Aerodynamics / Gas turbines / Fluid dynamics / Jet engines / Japan Aerospace Exploration Agency / Aircraft noise / Turbofan / Aircraft engine / Spaceflight / Aerospace engineering / Aviation

JAXA Aeronautics Magazine Institute of Aeronautical Technology 2013

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Source URL: www.aero.jaxa.jp

Language: English - Date: 2015-02-24 23:48:00
186Jet engines / Fluid dynamics / Turbines / Aerodynamics / Metrology / Gas turbine / Turbine blade / Turbine / Thermal power station / Technology / Energy / Mechanical engineering

Principal Research Results Performance Verification of X-ray CT for the Durability Assessment of Thermal Power Components Background It is very important to develop technologies in analytical durability assessment of th

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Source URL: criepi.denken.or.jp

Language: English - Date: 2010-02-04 23:04:36
187Jet engines / Chemical engineering / Heat pumps / Aerodynamics / Gas turbine / Turbine / Combustor / Engine / Fuel cell / Energy / Technology / Energy conversion

Base Technology Subjects Energy Engineering Research Laboratory Brief Overview Providing innovative fundamental technologies to the electric industry and the society, the Energy Engineering Research Laboratory (EERL) is

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Source URL: criepi.denken.or.jp

Language: English - Date: 2011-11-04 00:31:57
188Heat transfer / Physical quantities / Jet engines / Heat conduction / Thermodynamics / Thermal barrier coating / Combustor / Gas turbine / Turbine / Chemistry / Mechanical engineering / Physics

Principal Research Results Development of the Temperature Prediction Method for Hot Gas Path Parts of 1300 ℃ Class Gas Turbines Background Electric power companies are working to extend the remaining life of gas turbi

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Source URL: criepi.denken.or.jp

Language: English - Date: 2008-09-29 03:15:21
189Mechanical engineering / Gas compressor / Chemical engineering / Technology / Jet engines / Compressors / Underwater diving / Heating /  ventilating /  and air conditioning

DATE: July 2011 DESCRIPTION:

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Source URL: www.arbusa.com

Language: English - Date: 2013-10-22 14:14:37
190Technology / Fluid mechanics / Heating /  ventilating /  and air conditioning / Hydrogen compressor / Gas compressor / Jet engines / Hydrogen vehicle / Hydrogen production / Hydrogen station / Compressors / Mechanical engineering / Hydrogen technologies

Hydrogen Component Validation - DOE Hydrogen and Fuel Cells Program FY 2014 Annual Progress Report

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Source URL: www.hydrogen.energy.gov

Language: English - Date: 2014-11-10 15:41:46
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