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contributor authorC. J. Smith
date accessioned2017-05-08T23:50:06Z
date available2017-05-08T23:50:06Z
date copyrightApril, 1996
date issued1996
identifier issn1528-8919
identifier otherJETPEZ-26751#236_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116927
description abstractCosts 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.
publisherThe American Society of Mechanical Engineers (ASME)
titleAffordable Nacelle Technologies for Future Turbofans
typeJournal Paper
journal volume118
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2816582
journal fristpage236
journal lastpage239
identifier eissn0742-4795
keywordsFuels
keywordsEngines
keywordsDrag (Fluid dynamics)
keywordsLaminar flow
keywordsAircraft
keywordsWings AND Turbofans
treeJournal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 002
contenttypeFulltext


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