Affordable Nacelle Technologies for Future TurbofansSource: Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 002::page 236Author:C. J. Smith
DOI: 10.1115/1.2816582Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Costs are playing an ever-increasing role in determining what the next generation of aircraft and engines will be. In addition to deciding to what extent wing/engine integration or drag-reducing laminar flow technologies can be employed, etc., the economic impact on both aircraft operation and engines launch and development costs must be evaluated. SFC or fuel burn advantages are no longer dominant to the extent they used to be and for some apparently promising technology concepts the cost disadvantages outweigh the aerodynamic advantages when both effects are transposed into aircraft direct operating costs. In addition, a simple metric has been evolved to rank different technology concepts and prioritize them in order to help determine the most deserving technologies for scarce development funds.
keyword(s): Fuels , Engines , Drag (Fluid dynamics) , Laminar flow , Aircraft , Wings AND Turbofans ,
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contributor author | C. J. Smith | |
date accessioned | 2017-05-08T23:50:06Z | |
date available | 2017-05-08T23:50:06Z | |
date copyright | April, 1996 | |
date issued | 1996 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26751#236_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/116927 | |
description abstract | Costs are playing an ever-increasing role in determining what the next generation of aircraft and engines will be. In addition to deciding to what extent wing/engine integration or drag-reducing laminar flow technologies can be employed, etc., the economic impact on both aircraft operation and engines launch and development costs must be evaluated. SFC or fuel burn advantages are no longer dominant to the extent they used to be and for some apparently promising technology concepts the cost disadvantages outweigh the aerodynamic advantages when both effects are transposed into aircraft direct operating costs. In addition, a simple metric has been evolved to rank different technology concepts and prioritize them in order to help determine the most deserving technologies for scarce development funds. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Affordable Nacelle Technologies for Future Turbofans | |
type | Journal Paper | |
journal volume | 118 | |
journal issue | 2 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.2816582 | |
journal fristpage | 236 | |
journal lastpage | 239 | |
identifier eissn | 0742-4795 | |
keywords | Fuels | |
keywords | Engines | |
keywords | Drag (Fluid dynamics) | |
keywords | Laminar flow | |
keywords | Aircraft | |
keywords | Wings AND Turbofans | |
tree | Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 002 | |
contenttype | Fulltext |