Above certain Mach numbers, flows in wind tunnels can no longer fully simulate the actual flow physics. In the design of optimal propulsion systems, which are capable of economically propelling aircraft to hypersonic Mach numbers, understanding of the 'real' flow is mandatory. This paper will address recently developed numerical elements of an advanced CFD code in terms of computational speed and accuracy. Results will be presented of several calculations performed to gain insight into the flow in hypersonic intakes.


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    Title :

    CFD Contributions During Hypersonic Airplane Intake Design


    Contributors:
    N. C. Bissinger (author) / A. Eberle (author)

    Publication date :

    1992


    Size :

    24 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    CFD contributions during hypersonic airplane intake design

    Bissinger, N. C. / Eberle, Albrecht / Hubschrauber und Flugzeuge, Messerschmitt-Bölkow-Blohm GmbH, Ottobrunn | TIBKAT | 1991


    CFD Contributions During Hypersonic Airplane Intake Design

    N. C. Bissinger / A. Eberle | NTIS | 1991



    Structural Design for a Hypersonic Research Airplane

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