The paper discusses the structural design and analysis of a Mach zero to five turbo-ramjet propulsion system for a Mach five waverider-derived cruise vehicle. The level of analysis detail necessary for a credible conceptual design is shown. The results of a finite-element failure mode sizing analysis for the engine primary structure is presented. The importance of engine/airframe integration is also discussed.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Structural design and analysis of a Mach zero to five turbo-ramjet system


    Contributors:

    Conference:

    AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit ; 1993 ; Monterey, CA, United States


    Publication date :

    1993-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English






    AN EXPERIMENTAL INVESTIGATION OF TURBO-RAMJET ENGINE INTAKE AT MACH 4

    Raju, Nandhini / Pai, Tonse Gokuldas / Verma, S. B. et al. | TIBKAT | 2020


    An Experimental Investigation of Turbo-Ramjet Engine Intake at Mach 4

    Raju, Nandhini / Pai, Tonse Gokuldas / S B, Verma et al. | AIAA | 2020