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Rocket and propulsion systems research

36 ta ish

  1. CALCULATION OF HYDRAULIC RESISTANCE OF A TUBULAR-GRIDSE NOZZLE WITH SPIRAL TURBULIZERS

    Nurmukhamedov Habibulla Sagdullaevich, Mavlonov Elbek Tulkinovich, S.Kh. Nishonova +1

    MaqolaRocket and propulsion systems researchHimičeskaâ tehnologiâ. Kontrolʹ i upravlenie/Chemical Technology. Control and Management20240 iqtibos
    ABI

  2. Outflow of compressible fluid from a cylindrical nozzle

    A. Kh. Zakirov

    MaqolaRocket and propulsion systems researchAIP conference proceedings20240 iqtibos
    ABI

  3. Propulsive and Combustion Modelling of SABRE Engine in Rocket Mode to Support NOx Emissions Estimation in Conceptual Design

    Alessio Ricca, Valeria Borio, Roberta Fusaro +3

    MaqolaRocket and propulsion systems research20240 iqtibos
    ABI

  4. Inflatable Heat Shields Solutions for Hypersonic Re-entry Applications: the European Commission EFESTO-2 Project

    GUIDOTTI, Giuseppe, TOSO, Federico, A. Princi +16

    MaqolaGas Dynamics and Kinetic TheoryHAL (Le Centre pour la Communication Scientifique Directe)20240 iqtibos
    ABI

  5. Study on the Influence of Aeration Pipeline on the Hydraulic Performance of Rotary Refracting Nozzle

    Chilin Wei, Ruichao Hao, Delan Zhu +1

    PreprintRocket and propulsion systems researchSSRN Electronic Journal20240 iqtibos
    ABI

  6. Effects of mechanical heaving oscillation parameters on the flow and heat transfer characteristics of annular fuel elements

    Mingting Wu, Mingfei He, Yunlong Zhou +3

    MaqolaHeat transfer and supercritical fluidsOcean Engineering20250 iqtibos
    ABI

  7. Multi-objective Optimal Sizing Method for a Cruise Missile with Multi-phase Missions

    Seongjoong Park, Ki-Jun Byeon, Yeonju Choi +4

    MaqolaGuidance and Control SystemsInternational Journal of Aeronautical and Space Sciences20250 iqtibos
    ABI

  8. Mathematical research on influence of geometric characteristics of centrifugal nozzle on its efficiency

    Борис Иванов, Asilkhuzha Ortikkhuzhayev, Humoyun Gafforov +3

    MaqolaRanque-Hilsch vortex tubeAIP conference proceedings20250 iqtibos
    ABI

  9. Using a predictive surrogate model for hydrogen mixing estimation in scramjet engine with strut configurations

    Zakarya Ahmed, Rassol Hamed Rasheed, Pooya Ghodratallah +5

    MaqolaRocket and propulsion systems researchJournal of the Brazilian Society of Mechanical Sciences and Engineering20260 iqtibos
    ABI

  10. GKU JAXA Contact

    Yoshimitsu Katayama

    PreprintRocket and propulsion systems researchZenodo (CERN European Organization for Nuclear Research)20260 iqtibos
    ABI

  11. GKU JAXA Contact

    Yoshimitsu Katayama

    PreprintRocket and propulsion systems researchZenodo (CERN European Organization for Nuclear Research)20260 iqtibos
    ABI