IAI (Israel Aircraft Industries) has initiated a program to have its own capability in experimental hypersonic aerodynamics. It is planning to reconstruct and operate the Hypersonic Wind Tunnel, purchased in 1978 from General Dynamics, together with its Tri-sonic Wind Tunnel to complement its Low Speed and High Speed Wind Tunnels. The air supply system, air heater, by-pass valve, nozzles, test chamber and diffuser-ejector system of the Hypersonic Wind Tunnel are described and its operational characteristics and experience presented. The purpose of the presentation is to invite participants' suggestions for future development of hypersonic vehicles.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    IAI Hypersonic Wind Tunnel


    Beteiligte:
    L. Y. Jacobi (Autor:in) / M. Zilberman (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Hypersonic Wind Tunnel Testing

    Brian R. Hollis | NTRS


    Hypersonic Wind Tunnel Testing

    B. R. Hollis | NTIS | 2022


    Radiatively Driven Hypersonic Wind Tunnel

    Miles, R. / Brown, G. / Lempert, W. et al. | British Library Conference Proceedings | 1994


    Radiatively Driven Hypersonic Wind Tunnel

    Miles, R.B. | Online Contents | 1995


    Hypersonic wind tunnel nozzle study

    SCAGGS, NORMAN / NEUMANN, RICHARD / LAGANELLI, ANTHONY | AIAA | 1992