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 Aircraft Eng v 31 n 361 Mar 1959 p 81-3; Engineering v 187 n 4848 Feb 6 1959 p 187-8; Aeroplane v 96 n 2473 Jan 23 1959 p 97-9)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    New A.R.A. supersonic wind tunnel


    Weitere Titelangaben:

    Engineer


    Erschienen in:

    Engineer ; 207 , n 5375


    Erscheinungsdatum :

    1959


    Format / Umfang :

    179 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