IGTC-49 MEASUREMENTS OF FLOW FIELD WITHIN AN AXIAL FLOW FAN ROTOR USING A LASER TWO FOCUS VELOCIMETER(Session B-3 Aerodynamics III (Turbomachinery))

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概要

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• The flow field within the rotor of a transonic axial flow fan has been investigated in the tip region by using a Laser Two Focus velocimeter. The tests were carried out at design speed and mass flow corresponding to the point of maximum efficiency. The flow phenomena investigated include the flow variation from passage to passage, the shock intensity, the three-dimensionality of the shock in the blade passage and the shock boundary layer interaction.

• 公益社団法人日本ガスタービン学会の論文

著者

• Yasu S.

  Aero-engine Operations Ishikawajima-harima Heavy Industries

• Nagano S.

  Aero-engine Operations Ishikawajima-harima Heavy Industries

• Tamaki T.

  Aero-Engine Operations, Ishikawajima-Harima Heavy Industries

• Tamaki T.

  Aero-engine Operations Ishikawajima-harima Heavy Industries

• Tamaki T.

  Aero-engine & Space Operations Ihi

関連論文

• IGTC-49 MEASUREMENTS OF FLOW FIELD WITHIN AN AXIAL FLOW FAN ROTOR USING A LASER TWO FOCUS VELOCIMETER
• IGTC-49 MEASUREMENTS OF FLOW FIELD WITHIN AN AXIAL FLOW FAN ROTOR USING A LASER TWO FOCUS VELOCIMETER(Session B-3 Aerodynamics III (Turbomachinery))
• IGTC-43 Premixing Prevaporizing Fuel Injector for Low NO_x Combustor(Session B-6 COMBUSTION I)

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