contributor author | K. Suzuki | |
contributor author | A. Ishii | |
contributor author | T. Saito | |
contributor author | M. Matsuki | |
contributor author | T. Torisaki | |
contributor author | S. Horiuchi | |
date accessioned | 2017-05-08T23:04:47Z | |
date available | 2017-05-08T23:04:47Z | |
date copyright | January, 1978 | |
date issued | 1978 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26739#129_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/91033 | |
description abstract | Research on a high-pressure combustor for turbofan engines has been carried out at National Aerospace Laboratory (Tokyo). In the first step, a design point of research combustor was fixed from a initial program of FJR Turbofan development. Then the combustor-type was developed, and the major dimensions were decided mainly from the experiences of JR-series lift jet engines, and partly from published data. As the next step, various-segment-type and full-annular-type combustors were tested at the pressure up to 15 bar. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Design and Development of a High-Pressure Combustor for Aero-Gas-Turbines | |
type | Journal Paper | |
journal volume | 100 | |
journal issue | 1 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.3446303 | |
journal fristpage | 129 | |
journal lastpage | 135 | |
identifier eissn | 0742-4795 | |
keywords | High pressure (Physics) | |
keywords | Combustion chambers | |
keywords | Design | |
keywords | Turbines | |
keywords | Turbofans | |
keywords | Jet engines | |
keywords | Aerospace industry | |
keywords | Pressure | |
keywords | Engines AND Dimensions | |
tree | Journal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 001 | |
contenttype | Fulltext | |