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机译:风洞测试中温度引起的光学传感器压力测量值的变化
Ecole de Technologie Superieure, Montreal, Quebec H3C 1K3, Canada Laboratory of Research in Active Controls, Avionics and AeroServoElasticity LARCASE, 1100 Notre-Dame West Street AIAA;
Ecole de Technologie Superieure, Montreal, Quebec H3C 1K3, Canada Laboratory of Research in Active Controls, Avionics and AeroServoElasticity LARCASE, 1100 Notre-Dame West Street AIAA;
National Research Council, Ottawa, Ontario K1A 0R6, Canada Institute of Aeronautical Research, Montreal Road, Uplands Building U66 AIAA;
Ecole de Technologie Superieure, Montreal, Quebec H3C 1K3, Canada Laboratory of Research in Active Controls, Avionics and AeroServoElasticity LARCASE, 1100 Notre-Dame West Street AIAA;
C_p:pressure coefficient; c: chord; M: Mach number; N: natural logarithm of rapport between amplified perturbation and initial perturbation in laminar flow; N_(cr): N critical, the value of N when transition between laminar and turbulent flow occurs; et al;
机译:风洞试验光压测量中三角网的整流控制点选择方法
机译:用于温度和压力测量的碳化硅光学传感器响应去耦
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机译:传感器形状对风隧道试验确认振荡压力测量的影响
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机译:具有温度补偿的单片结构光纤传感器用于压力测量
机译:使用光PM-FBG传感器进行应变独立温度测量的证明,用于卫星面板的地面测试