This paper describes the technical features of the Thrust Vectoring Nozzle (TVN) developed by ITP and its advantages for modem military aircraft. It is presented in Conjunction with two other papers by DASA (Thrust Vectoring for Advanced Fighter Aircraft High Angle of Attack Intake Investigations) and MTU- Muenchen (Integrated Thrust Vector Jet Engine Control) respectively.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Thrust Vectoring Nozzle for Modern Military Aircraft


    Beteiligte:
    D. Ikaza (Autor:in)

    Erscheinungsdatum :

    2000


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Thrust Vectoring Nozzle for Military Aircraft Engines

    Ikaza, D. / Zarda, P.R. / Ruiz, C.G. et al. | British Library Conference Proceedings | 2000


    Fluid thrust vectoring nozzle and wing integrated aircraft

    PENG QIAN / GU YUNSONG / HUANG ZI et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    THRUST VECTORING EXHAUST NOZZLE FOR AIRCRAFT PROPULSION SYSTEM

    HANRAHAN PAUL R / BOCHAR ROXANNE M | Europäisches Patentamt | 2023

    Freier Zugriff


    Thrust-Vectoring Nozzle Performance Modeling

    Erich A. Wilson / Dan Adler / Pinhas Bar-Yoseph | AIAA | 2003