Stall-Flutter in Cascade : 2nd Report, Translatory Vibration of Cascade Blades as Treated by Semi-Actuator Disc Method, Part 2

スポンサーリンク

概要

• 論文の詳細を見る

• In the 1st report fundamental equations for calculating the aerodynamic force acting on the cascading blades vibrating in a translatory mode were given. This report shows the results of the calculation and gives the criterion for the flutter (the boundary of the region where the aerodynamic damping force cannot be negative).

• 一般社団法人日本機械学会の論文

著者

• Okazaki Takuro

  Faculty Of Engineering University Of Tokyo

• TANIDA Yosimiti

  Aeronautical Research Institute, University of Tokyo

• Tanida Yosimiti

  Aeronautical Research Institute University Of Tokyo

関連論文

• Jet Noise : Far Noise Field of Subsonic Free Air Jet
• Jet Noise : 3rd Report, Effect of the Shape of Nozzle-Exit
• Jet Noise : 2nd Report, Effect of Shear on the Noise of a Jet
• Stall-Flutter in Cascade : 2nd Report, Translatory Vibration of Cascade Blades as Treated by Semi-Actuator Disc Method, Part 2
• Stall-Flutter in Cascade : 3rd Report, Arbitrary Mode Vibration of Cascade Blades as Treated by Semi-Actuator Disc Method
• Acoustic Characteristics of Orifice Holes Exposed to Grazing Flow
• Stall-Flutter in Cascade : 1st Report, Translatory Vibration of Cascade Blades as Treated by Semi-Actuator Disc Method, Part 1
• Experimental Study on Flutter in Cascading Blades : 1st Report, Measurement of the Aerodynamic Damping Force Acting on Cascading Blades Vibrating in Translatory Mode

スポンサーリンク