Topics in aerospace research are presented. They include theoretical and experimental performance of a dual mode ramjet for the Mach 3.5 to 7 domain of flight velocities, time dependent methods for computing wall effects in two-dimensional supercritical flow, analog (rheoelectrical) simulation of the small perturbation equation for transonic flows, determination of the dynamic characteristics of an aircraft structure, and a piston unit for rate modulation of a liquid propellant flow.


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    Title :

    Aerospace Research


    Publication date :

    1974


    Size :

    123 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English