Development of propulsion system can be divided into three periods: reciprocating power plant; air breathing reaction power plant; rocket propulsion power plant; more knowledge of combustion is necessary; extended theory of elasticity to be applied to design of turbine blading needed; diagrams show speed range of various power plants at sea level, 20,000, 40,000, 60,000 and 80,000 ft.


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    Titel :

    Research challenge in aircraft propulsion for universities


    Weitere Titelangaben:

    J Eng Education


    Beteiligte:
    Stoeckly, E.E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1948


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Research challenge in aircraft propulsion

    Stoeckly, E.E. | Engineering Index Backfile | 1948



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    Koschel, W. W. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1998



    Nasa Research in Aircraft Propulsion

    M. A. Beheim | NTIS | 1982