pone.0298113.s001.docx (16.76 kB)
Hot experimental technique with electrical heating device in impulse-type facility.
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posted on 2024-02-14, 18:29 authored by Sungmo Yang, Ilsung Choi, Gisu ParkHot experimental technique with electrical heating device in impulse-type facility.
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induced shape change99 ± 010 mm diametersmach 5 flightflight objects encounteredhemisphere model constructedcone model manufacturedjet tunnel provideddiv >< p2 supcombined test facilityshock tunnel usedshock tunneljet tunnelcombined testhypersonic flighttest modelfacility utilizingpreheated modelfaced modeltest proceduresvalidated duesurface roughnesssts303 materialsecond experimentscale huelsrelated changespressure altitudematerial modelsinvestigated usingintegrated setupindividual partshowever preheatinghot surfacesheat fluxflow conditionfirst experimententhalpy flowdeveloped usingal6061 materialaerothermodynamic testingaerothermodynamic phenomenaaerodynamic heating24 km03 mw
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