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NASA-CR-152141

Prop-fan data support study

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1978

Abstract: Updated parametric prop-fan data packages are presented and the rationale used in developing the new prop-fan data is detailed. These data represent Hamilton Standard's projections of prop-fan characteristics for aircraft that are expected to be in-service in the 1985 to 1990 time frame. The basic prop-fan configuration was designed for efficient cruise operation at 0.8 Mach number and 10,668M altitude. The design blade tip speed is 244 mps and the design power loading is 301 KW/M squared.
URI: https://yse.yabesh.ir/std/handle/yse/127198
Subject: AERODYNAMIC
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    NASA-CR-152141

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:03:34Z
date available2017-09-04T17:03:34Z
date copyright01/01/1978
date issued1978
identifier otherXXMKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/127198
description abstractUpdated parametric prop-fan data packages are presented and the rationale used in developing the new prop-fan data is detailed. These data represent Hamilton Standard's projections of prop-fan characteristics for aircraft that are expected to be in-service in the 1985 to 1990 time frame. The basic prop-fan configuration was designed for efficient cruise operation at 0.8 Mach number and 10,668M altitude. The design blade tip speed is 244 mps and the design power loading is 301 KW/M squared.
languageEnglish
titleNASA-CR-152141num
titleProp-fan data support studyen
typestandard
page111
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1978
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRCRAFT
subject keywordsCHARACTERISTICS
subject keywordsCOST
subject keywordsDATA
subject keywordsDESIGN
subject keywordsENGINE
subject keywordsESTIMATES
subject keywordsFANS
subject keywordsFORECASTING
subject keywordsNOISE
subject keywordsPERFORMANCE
subject keywordsPREDICTION
subject keywordsPROPELLER
subject keywordsTABLES
subject keywordsTECHNOLOGICAL
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