With the resurgence of interest in high supersonic and hypersonic flight there is a need to simulate airbreathing engines which may be used in this flight regime. To meet this requirement the RAMSCRAM code was developed. The code calculates 1-D flow properties at each component interface and the overall performance of the engine. It uses equilibrium thermodynamics which accounts for dissociation and allows for any fuel or combination of fuels. The program can simulate ramjet, scramjet, rocket, and ducted rocket engines.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    RAMSCRAM: A flexible ramjet/scramjet engine simulation program


    Contributors:

    Conference:

    International Gas Turbine Aeroengine Congress and Exposition ; 1990 ; Brussels, Belgium


    Publication date :

    1990-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Ramjet and Scramjet Engine

    Babu, V. | Springer Verlag | 2021




    LARGE EDDY SIMULATION OF RAMJET TO SCRAMJET TRANSITION

    Nilsson, T. / Fureby, C. | British Library Conference Proceedings | 2022


    Scramjet Engine Tests at Ramjet Engine Test Facility in JAXA-KSPC

    Tomioka, Sadatake / Ueda, Shuuichi / Tani, Kohichiro et al. | AIAA | 2007