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    The Development of the Whittle Turbojet

    Source: Journal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 002::page 249
    Author:
    C. B. Meher-Homji
    DOI: 10.1115/1.2818112
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Sir Frank Whittle passed away on August 8, 1996, at the age of 89, in Maryland. His work in developing the turbojet can truly be said to represent one of the greatest mechanical engineering achievements in the last 70 years. The development of the turbojet demanded that Whittle face almost insurmountable technical and institutional challenges. The technical challenges included developing centrifugal compressor pressure ratios of 4:1 from the prevailing technology level of 2.5:1, increasing compressor efficiencies from 65 to 80 percent while designing for combustion intensities that were 10 times the prevailing state of the art in boiler technology. He was also responsible for utilizing a vortex turbine design approach. The institutional challenges that he faced included changing a paradigm on aircraft propulsion technology and nurturing Power Jets Ltd. to produce excellent engine designs with minimal resources in terms of money, technical manpower, and governmental support. It is the object of this paper to document the epic long-drawn-out struggle fought by Sir Frank against entrenched technical opinion, which ultimately resulted in the turbojet revolution. The technical aspects of his pioneering work with emphasis on the problems he encountered will also be discussed.
    keyword(s): Turbojets , Compressors , Design , Turbines , Vortices , Engine design , Jets , Boilers , Pressure , Combustion , Mechanical engineering AND Aircraft propulsion ,
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      The Development of the Whittle Turbojet

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    https://yetl.yabesh.ir/yetl1/handle/yetl/120427
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorC. B. Meher-Homji
    date accessioned2017-05-08T23:56:35Z
    date available2017-05-08T23:56:35Z
    date copyrightApril, 1998
    date issued1998
    identifier issn1528-8919
    identifier otherJETPEZ-26778#249_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/120427
    description abstractSir Frank Whittle passed away on August 8, 1996, at the age of 89, in Maryland. His work in developing the turbojet can truly be said to represent one of the greatest mechanical engineering achievements in the last 70 years. The development of the turbojet demanded that Whittle face almost insurmountable technical and institutional challenges. The technical challenges included developing centrifugal compressor pressure ratios of 4:1 from the prevailing technology level of 2.5:1, increasing compressor efficiencies from 65 to 80 percent while designing for combustion intensities that were 10 times the prevailing state of the art in boiler technology. He was also responsible for utilizing a vortex turbine design approach. The institutional challenges that he faced included changing a paradigm on aircraft propulsion technology and nurturing Power Jets Ltd. to produce excellent engine designs with minimal resources in terms of money, technical manpower, and governmental support. It is the object of this paper to document the epic long-drawn-out struggle fought by Sir Frank against entrenched technical opinion, which ultimately resulted in the turbojet revolution. The technical aspects of his pioneering work with emphasis on the problems he encountered will also be discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Development of the Whittle Turbojet
    typeJournal Paper
    journal volume120
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2818112
    journal fristpage249
    journal lastpage256
    identifier eissn0742-4795
    keywordsTurbojets
    keywordsCompressors
    keywordsDesign
    keywordsTurbines
    keywordsVortices
    keywordsEngine design
    keywordsJets
    keywordsBoilers
    keywordsPressure
    keywordsCombustion
    keywordsMechanical engineering AND Aircraft propulsion
    treeJournal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 002
    contenttypeFulltext
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