Fighter aircraft dealt with whose normal duty would be to 'stand off' at modest flight speeds and achieve high supersonic speeds only during combat; arrangement where heat is retained in 'pipe line' until fuel is discharged to engine, not allowing any fuel to return to low pressure zones; suitability of two-circuit spill system as heat sink for supply of fuel directly to combustion chamber; effect of fuel temperature on gas turbine control systems.


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    Titel :

    Fuel systems and high speed flight


    Weitere Titelangaben:

    Shell Aviation News


    Beteiligte:
    Tyler, S.R. (Autor:in) / Turner, H.G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1957


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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