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Electrical Control of a Semiconductor Heater for a Continuous Mach 7 True- Temperature Wind Tunnel

机译：连续马赫数为7的真温风洞的半导体加热器的电气控制

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《AIAA Aerodynamic Measurement Technology and Ground Testing Conference 》|2004年|P.1-9|共9页
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H. Frederick;
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中图分类空气动力学 ;
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2. Hydrogen-fueled detonation ramjet model: Wind tunnel tests at approach air stream Mach number 5.7 and stagnation temperature 1500 K [J] . Frolov S. M., Zvegintsev V. I., Ivanov V. S., International journal of hydrogen energy . 2018 ,第15期

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4. Electrical Control of a Semiconductor Heater for a Continuous Mach 7 True- Temperature Wind Tunnel [C] . American Institute of Aeronautics and Astronautics Aerodynamic Measurement Technology and Ground Testing Conference . 2004

机译：用于连续马赫7的半导体加热器的电气控制真正温度风隧道
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Electrical Control of a Semiconductor Heater for a Continuous Mach 7 True- Temperature Wind Tunnel

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