Future aircraft with the capability of short takeoff and landing, and improved maneuverability especially in the post-stall flight regime will incorporate exhaust nozzles which can be thrust vectored. In order to conduct thrust vector research in the Mechanical Engineering Department at Cal Poly, a program was planned with two objectives; design and construct a multicomponent thrust stand for the specific purpose of measuring nozzle thrust vectors; and to provide quality low moisture air to the thrust stand for cold flow nozzle tests. The design and fabrication of the six-component thrust stand was completed. Detailed evaluation tests of the thrust stand will continue upon the receipt of one signal conditioning option (-702) for the Fluke Data Acquisition System. Preliminary design of thrust nozzles with air supply plenums were completed. The air supply was analyzed with regard to head loss. Initial flow visualization tests were conducted using dual water jets.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design and Evaluation of Thrust Vectored Nozzles Using a Multicomponent Thrust Stand


    Beteiligte:
    T. W. Carpenter (Autor:in) / E. W. Blattner (Autor:in) / R. E. Stagner (Autor:in) / J. Contreras (Autor:in) / D. Lencioni (Autor:in)

    Erscheinungsdatum :

    1990


    Format / Umfang :

    63 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Design and evaluation of thrust vectored nozzles using a multicomponent thrust stand

    Carpenter, Thomas W. / Blattner, Ernest W. / Stagner, Robert E. et al. | NTRS | 1990


    THRUST VECTORED MULTICOPTERS

    KHOO SUI YANG / NORTON MICHAEL JOHN / KOUZANI ABBAS ZAHEDI | Europäisches Patentamt | 2019

    Freier Zugriff

    THRUST VECTORED MULTICOPTERS

    KHOO SUI YANG / NORTON MICHAEL JOHN / KOUZANI ABBAS ZAHEDI | Europäisches Patentamt | 2022

    Freier Zugriff

    Thrust vectored multicopters

    KHOO SUI YANG / NORTON MICHAEL JOHN / KOUZANI ABBAS ZAHEDI | Europäisches Patentamt | 2022

    Freier Zugriff

    Thrust vectored multicopters

    KHOO SUI YANG / NORTON MICHAEL JOHN / KOUZANI ABBAS ZAHEDI | Europäisches Patentamt | 2021

    Freier Zugriff