Problem of charge air cooling in aircraft discussed and it is shown that it is complicated by necessity for achieving cooling unit of low weight and small volume; method of obtaining low cooler weight by using high heat transfer known to exist in region adjacent to leading edge of surface is proposed and details given of experiments carried out to exploit its possibilities.


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    Titel :

    Heat transfer performance of louver surfaces and their application to aircraft intercoolers


    Weitere Titelangaben:

    Australian Council Aeronautics -- Report


    Beteiligte:
    Barna, P.S. (Autor:in)


    Erscheinungsdatum :

    1946


    Format / Umfang :

    19 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Intercoolers and their performance in Aircraft

    Anderson, S.K. / Scherer, P.A. | Engineering Index Backfile | 1943



    Generalized selection charts for harrison and tubular intercoolers

    Wood, G.P. / Tifford, A.N. | Engineering Index Backfile | 1942


    High-altitude cooling ; 4: Intercoolers

    Rubert, K. F. | TIBKAT | 1944


    NEW ONE-DIMENSIONAL FLUID-DYNAMIC MODEL FOR AUTOMOTIVE INTERCOOLERS

    Galindo, J. / Serrano, J. R. / Climent, H. et al. | British Library Conference Proceedings | 2001