A basic requirement of the test facility is to apply as far as possible flight conditions to the tested rocket engine [10]. It is mandatory that all interfaces between the bench and the engine are adjusted to the same values as on the launcher. Furthermore the evolution of interface parameters versus the time is regulated according the evolution during flight.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Simulation of Flight Conditions


    Additional title:

    Springer Aerospace Techn.


    Contributors:


    Publication date :

    2010-08-20


    Size :

    10 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English





    In-Flight Ice Accretion Simulation in SLD Conditions

    Sabri, Farhad / Trifu, Octavian / Paraschivoiu, Ion | AIAA | 2007


    Quad-Rotor Flight Simulation in Realistic Atmospheric Conditions

    Davoudi, Behdad / Taheri, Ehsan / Duraisamy, Karthik et al. | AIAA | 2020


    In-Flight Ice Accretion Simulation in SLD Conditions

    Sabri, F. / Trifu, O. / Paraschivoiu, I. et al. | British Library Conference Proceedings | 2007


    DSMC Simulation of Ablating Microstructures at Flight Relevant Conditions

    Ramjatan, Sahadeo / Kroells, Michael D. / Schwartzentruber, Thomas E. | AIAA | 2021