A brief account of research activities on problems related to air-breathing propulsion is made in this final report for the step funded research grant NASA NGL 14-005-140. Problems include the aircraft ejector-nozzle propulsive system, nonconstant pressure jet mixing process, recompression and reattachment of turbulent free shear layer, supersonic turbulent base pressure, low speed separated flows, transonic boattail flow with and without small angle of attack, transonic base pressures, Mach reflection of shocks, and numerical solution of potential equation through hodograph transformation.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Fluid Dynamic Problems Associated with Air-Breathing Propulsive Systems


    Contributors:
    W. L. Chow (author)

    Publication date :

    1979


    Size :

    51 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    Comparison of different propulsive systems for air-breathing launcher

    Lepelletier, Max / Zendron, Remy / Bellande, Patrick et al. | AIAA | 1995


    STRUCTURE FOR PROPULSIVE AIRCRAFT ASSEMBLY, ASSOCIATED PROPULSIVE SYSTEM AND ASSEMBLY

    RAVISE FLORIAN / MENAY HASSAN | European Patent Office | 2018

    Free access

    Preliminary study of propulsive fluid accumulator systems

    Demetriades, S.T. | Engineering Index Backfile | 1962