Stability limit of supermulti-jets convergence engine operated from startup to extremely-hypersonic conditions: Revealed by shock-tube experimens

Ken Naitoh, Dai Shimizu, Shouhei Nonaka

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    19 Citations (Scopus)

    Abstract

    Shock tube experiments reveal whether or not the single lightweight compression system of the supermultijets colliding with pulsation for aircars and aircraftsworks stably, which was proposed based on our previous three-dimensional unsteady computations. This compression system essentially differs from those in the traditional four types of engines with piston, turbofan, ran-scram, and pulse-detonation, because of the supermulti-jets colliding. The single compression system is capable of operating over a wide range of Mach numbers from startup to the hypersonic regime. Shocktube experiments clarify the stability range of this system in detail. Influence of the number of supermulti-jets on the stability will also be examined. This system can also be extended with a special piston and scram jet systems to achieve an improved fuel consumption rate at various situations between the ground and the space, while maintaining a low noise level and also solving the problem of the buzz at highersonic conditions.

    Original languageEnglish
    Title of host publication18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012
    Publication statusPublished - 2012
    Event18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012 - Tours
    Duration: 2012 Sep 242012 Sep 28

    Other

    Other18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012
    CityTours
    Period12/9/2412/9/28

    Fingerprint

    Plant startup
    Shock tubes
    hypersonics
    Hypersonic aerodynamics
    shock tubes
    engines
    engine
    compression
    Engines
    pistons
    Pistons
    turbofans
    fuel consumption
    Detonation
    detonation
    Fuel consumption
    Mach number
    low noise
    experiment
    Experiments

    ASJC Scopus subject areas

    • Space and Planetary Science
    • Aerospace Engineering
    • Control and Systems Engineering

    Cite this

    Naitoh, K., Shimizu, D., & Nonaka, S. (2012). Stability limit of supermulti-jets convergence engine operated from startup to extremely-hypersonic conditions: Revealed by shock-tube experimens. In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012

    Stability limit of supermulti-jets convergence engine operated from startup to extremely-hypersonic conditions : Revealed by shock-tube experimens. / Naitoh, Ken; Shimizu, Dai; Nonaka, Shouhei.

    18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012. 2012.

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Naitoh, K, Shimizu, D & Nonaka, S 2012, Stability limit of supermulti-jets convergence engine operated from startup to extremely-hypersonic conditions: Revealed by shock-tube experimens. in 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, 12/9/24.
    Naitoh K, Shimizu D, Nonaka S. Stability limit of supermulti-jets convergence engine operated from startup to extremely-hypersonic conditions: Revealed by shock-tube experimens. In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012. 2012
    Naitoh, Ken ; Shimizu, Dai ; Nonaka, Shouhei. / Stability limit of supermulti-jets convergence engine operated from startup to extremely-hypersonic conditions : Revealed by shock-tube experimens. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012. 2012.
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