2-ft 6-in.×2-ft 3-in. tunnel, for speeds ranging from Mach 1.4 to 3.5, completed at Aircraft Research Assn, Bedford; tunnel is driven by 13,750-hp axial compressor which also serves to evacuate ventilated working section of transonic tunnel. (see also Engineering v 187 n 4848 Feb 6 1959 p 187-8; Engineer v 207 n 5375 Jan 30 1959 p 179; Aeroplane v 96 n 2473 Jan 23 1959 p 97-99)


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    Titel :

    New A.R.A. supersonic wind tunnel


    Weitere Titelangaben:

    Aircraft Eng


    Erschienen in:

    Erscheinungsdatum :

    1959


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    New A.R.A. supersonic wind tunnel

    Engineering Index Backfile | 1959


    New A.R.A. supersonic wind tunnel

    Engineering Index Backfile | 1959


    New A.R.A. supersonic wind tunnel

    Engineering Index Backfile | 1959


    The New A.R.A. Supersonic Wind Tunnel

    Emerald Group Publishing | 1959


    A.R.A. holds ninth meeting and fifth exhibit

    Engineering Index Backfile | 1928