Time-accurate Experimental Investigation of Hypersonic Inlet Buzz at Mach 5

2020 
Hypersonic inlet buzz is investigated experimentally in a ramjet intake at Mach 5. A two-dimensional planar inlet featuring a double-compression ramp with 10 and 22° inclination to the freestream d...
    • Correction
    • Source
    • Cite
    • Save
    • Machine Reading By IdeaReader
    17
    References
    8
    Citations
    NaN
    KQI
    []