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Hagenmaier et al., 2016 - Google Patents

Computational Analysis of Flow Phenomena in a Back-Pressured Supersonic Isolator

Hagenmaier et al., 2016

Document ID
4576981788268319301
Author
Hagenmaier M
Hassan E
Publication year
Publication venue
52nd AIAA/SAE/ASEE Joint Propulsion Conference

External Links

Snippet

HE isolator is a constant (or nearly-constant) area duct located between the supersonic inlet and the combustor in a scramjet. Its function is to prevent the pressure caused by combustion from moving upstream and unstarting the inlet. This pressure isolation is …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5009Computer-aided design using simulation
    • G06F17/5018Computer-aided design using simulation using finite difference methods or finite element methods
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5009Computer-aided design using simulation
    • G06F17/504Formal methods
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5086Mechanical design, e.g. parametric or variational design
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F2217/00Indexing scheme relating to computer aided design [CAD]
    • G06F2217/16Numerical modeling

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