지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
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Abstract ⅰTable of Contents iiiList of Tables ⅴList of Figures ⅵNomenclature ⅷ1. Introduction 11.1 Background 11.2 Hypersonic flow field around flight vehicle 11.3 Aero-optics 21.4 Previous study 31.5 Research objectives 42. Experimental setup 62.1 Facility 62.1.1 Conical nozzle 82.1.2 Contoured nozzle 92.2 Model design and installation 102.2.1 Laser 122.2.2 Optical components 122.2.3 Sensor 152.2.4 Model 172.3 Measurement 192.3.1 Aero-optics measurement 192.3.2 Hypersonic flow field measurement 222.3.3 Measurement trigger system 253. Experiments results 283.1 Aero-optical characteristics in static flow 283.1.1 Experiment using wedged window 283.1.2 Experiment using hot wire 303.2 Hypersonic flow field characteristics 333.2.1 Shock tunnel performance validation 333.2.2 Nozzle flow characteristics 353.3 Aero-optical characteristics in hypersonic flow field 424. Conclusion 47Bibliography 48
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