Study of Transonic Cascade Airfoils by a Panel Method : Series B : Fluids Engineering, Heat Transfer, Combustion, Power, Thermophysical Properties

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概要

• 論文の詳細を見る
• 一般社団法人日本機械学会の論文
• 1987-08-15

著者

• Kaji Shojiro

  Department Of Aeronautics And Astronautics University Of Tokyo

• Kaji Shojiro

  Department Of Aeronautics University Of Tokyo

• SATO Iwataro

  Gas Turbine Design Section, Toshiba Corporation

• Sato Iwataro

  Gas Turbine Design Section Toshiba Corporation

• Kaji Shojiro

  Department Of Aeronautics And Astronautics Faculty Of Engineering The University Of Tokyo

関連論文

• The Effects of Aspect Ratio of a Finite Length Slit on the Mixing in the Three-Dimensional Supersonic Flow
• Acoustic Characteristics of Orifice Holes Exposed to Grazing Flow
• The Two-Dimensional Supersonic Flow and Mixing Field with a Perpendicular Injection
• Study on the Swirling Flow Field in a Rotating Cylinder : Numerical Analysis
• Study of Transonic Cascade Airfoils by a Panel Method : Series B : Fluids Engineering, Heat Transfer, Combustion, Power, Thermophysical Properties
• Theoretical Study on the Unsteady Aerodynamic Characteristics of an Oscillating Cascade with Tip Clearance (In the Case of a Nonloaded Cascade)
• Theoretical Study on the Unsteady Aerodynamic Characteristics of an Oscillating Cascade with Tip Clearance : In the Case of Loaded Cascade
• Experimental Study on Unsteady Aerodynamic Characteristics of an Oscillating Cascade with Tip Clearance
• The Injection Methods and Mixing Characteristics in the Two-Dimensional Supersonic Free Stream
• The Three-Dimensional Supersonic Flow and Mixing Fields with a Perpendicular Air Injection from a Finite Length Slit
• The Effects of Acoustically Lined Walls on Cascade Flutter

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