The research project reported herein extended over a period from October 1997 through August 1999. The research resulted in three technical papers presented at the AIAA/SAE/ASME/ASEE 35th Joint Propulsion Conference in Los Angeles in July 1999. These three papers are attached to this Executive Summary to constitute the final report. Objective: The objective of this research was to determine the mixing characteristics between the primary rocket jets and the turbine exhaust stream in a simulated Rocket Based Combined Cycle propulsion concept operating in the air augmented rocket mode.


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    Title :

    RBCC Mixing Studies: Ejector Ramjet Design Optimization


    Publication date :

    1999


    Size :

    39 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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