Under the Propulsion Discipline of NASA s Fundamental Aeronautics Program s Hypersonics Project, a test apparatus, for testing a scramjet isolator model, is being constructed at NASA's Langley Research Center. The test apparatus will incorporate a 1-inch by 2-inch by 15-inch-long scramjet isolator model supplied with 2.1 lbm/sec of unheated dry air through a Mach 2.5 converging-diverging nozzle. The planned research will incorporate progressively more challenging measurement techniques to characterize the flow field within the isolator, concluding with the application of the Laser-Induced Thermal Acoustic (LITA) measurement technique. The primary goal of this research is to use the data acquired to validate Computational Fluid Dynamics (CFD) models employed to characterize the complex flow field of a scramjet isolator. This paper describes the test apparatus being constructed, pre-test CFD simulations, and the LITA measurement technique.


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    Titel :

    Laser-Induced Thermal Acoustic Measurements in a Highly Back-Pressured Scramjet Isolator Model: A Research Plan


    Beteiligte:

    Kongress:

    55th JANNAF Propulsion Meeting/42nd Combustion/30th Airbreathing Propulsion/30th Exhaust Plume Technology/24th Propulsion Systems Hazards/12th SPIRITS User Group Joint Subcommittee Meeting ; 2008 ; Newton, MA, United States


    Erscheinungsdatum :

    2008-05-12


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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

    Hagenmaier, Mark A. / Hassan, Ezeldin A. | AIAA | 2016


    Analysis of Hybrid LES / RANS Simulations of a Back-Pressured Supersonic Isolator

    Boles, John / Hagenmaier, Mark / Hsu, Kuang-Yu | AIAA | 2011


    Laser-Induced Thermal Acoustics (LITA) Measurements in a Scramjet Combustion Chamber: A Research Plan

    Forster, F. / Hell, A. / Weigand, B. et al. | British Library Conference Proceedings | 2013


    Unstart in an Axisymmetric Scramjet Isolator

    Kato, Nozomu / Im, Seong-kyun | AIAA | 2019


    Downstream pressure variation induced hysteresis in the scramjet isolator

    Huang, TingLong / Lianjie, Yue / Ma, Shenghu et al. | AIAA | 2017