amateur 发表于 2025-3-21 18:39:33
书目名称New Trends in Instrumentation for Hypersonic Research影响因子(影响力)<br> http://impactfactor.cn/if/?ISSN=BK0665962<br><br> <br><br>书目名称New Trends in Instrumentation for Hypersonic Research影响因子(影响力)学科排名<br> http://impactfactor.cn/ifr/?ISSN=BK0665962<br><br> <br><br>书目名称New Trends in Instrumentation for Hypersonic Research网络公开度<br> http://impactfactor.cn/at/?ISSN=BK0665962<br><br> <br><br>书目名称New Trends in Instrumentation for Hypersonic Research网络公开度学科排名<br> http://impactfactor.cn/atr/?ISSN=BK0665962<br><br> <br><br>书目名称New Trends in Instrumentation for Hypersonic Research被引频次<br> http://impactfactor.cn/tc/?ISSN=BK0665962<br><br> <br><br>书目名称New Trends in Instrumentation for Hypersonic Research被引频次学科排名<br> http://impactfactor.cn/tcr/?ISSN=BK0665962<br><br> <br><br>书目名称New Trends in Instrumentation for Hypersonic Research年度引用<br> http://impactfactor.cn/ii/?ISSN=BK0665962<br><br> <br><br>书目名称New Trends in Instrumentation for Hypersonic Research年度引用学科排名<br> http://impactfactor.cn/iir/?ISSN=BK0665962<br><br> <br><br>书目名称New Trends in Instrumentation for Hypersonic Research读者反馈<br> http://impactfactor.cn/5y/?ISSN=BK0665962<br><br> <br><br>书目名称New Trends in Instrumentation for Hypersonic Research读者反馈学科排名<br> http://impactfactor.cn/5yr/?ISSN=BK0665962<br><br> <br><br>Wordlist 发表于 2025-3-21 21:30:57
Hot Experimental Technique: a New Requirement of Aerothermodynamicspical measurement problems, is pro-posed. Details of the technique, regarding the tunnel type, model and measurement techniques are discussed. A stepwise approach to the involved problems is suggested.START 发表于 2025-3-22 01:07:53
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Laser-Based Diagnostics for Hypersonic Flows shock tunnel. These methods have unique capabilities for nonintrusive measurements of flowfield properties such as temperature, species concentration, velocity, density and pressure, as well as quantities derived from these properties such as mass flux (product of velocity and mass density).mighty 发表于 2025-3-22 15:39:12
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Requirements for Facilities and Measurement Techniques to Support CFD Development for Hypersonic Airt for the design of hypersonic aircraft. Illustrations are given of recent success in combining experimental and direct numerical simulation in CFD model development and validation for hypersonic perfect gas flows.Shuttle 发表于 2025-3-22 22:34:09
Hermes Measurement Needs in Hot Facilitiess (very short time duration, high level of temperature, wide range in level of pressure…). They are required for post processing data analysis and validation of numerical codes. The paper describes the different parameters to be measured.figment 发表于 2025-3-23 03:49:15
Computation and Experimentation of Free Piston Shock Tunnels — Example of the Marseille Facilityigh enthalpy flows characteristic of the reentry phase of the Hermes european shuttle. Preliminary results of pressure measurements in the compression chamber are also presented and compared with computational data.埋葬 发表于 2025-3-23 08:00:17
Ground Test Facilities and Instrumentation for Aerothermal and Aero-Optical Studies of Hypersonic Ine and flowfield instrumentation that will be used to determine the aerothermal characteristics of the flowfield over the hypersonic vehicle is described. Finally we discuss the aero-optic instrumentation which is used to evaluate the optical degradation through the shock layer surrounding the vehicle.