![Heat transfer / Physical quantities / Jet engines / Heat conduction / Thermodynamics / Thermal barrier coating / Combustor / Gas turbine / Turbine / Chemistry / Mechanical engineering / Physics Heat transfer / Physical quantities / Jet engines / Heat conduction / Thermodynamics / Thermal barrier coating / Combustor / Gas turbine / Turbine / Chemistry / Mechanical engineering / Physics](https://www.pdfsearch.io/img/25ba5c2953d12b2425d503cb9ec63f83.jpg)
| Document Date: 2008-09-29 03:15:21 Open Document File Size: 225,36 KBShare Result on Facebook
City Amsterdam / Vienna / / Country Japan / Austria / United States / Netherlands / / Facility Combustor Inlet Film Cooling Air port Ratio / / IndustryTerm gas turbine / hot gas path parts / class gas turbine / / NaturalFeature Combustor Inlet / / Organization Energy Engineering Research Laboratory / / Person Masahiko Morinaga / Toshihiko Takahashi / / Position Research Scientist / Thermal Engineering Sector / Research Scientist / Advanced Power Engineering Sector / / ProvinceOrState Hawaii / / Technology Fluid Dynamics / heat transfer / Simulation / /
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