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Measurements of air loading on extension plates set at the trailing edge of the Gottingen 797 aerofoil section at a Reynolds number of 3 x 10⁵

Measurements of air loading on extension plates set at the trailing edge of the Gottingen 797 aerofoil section at a Reynolds number of 3 x 10⁵
紙記事
Akira ITO<Z14-1679>明治大学理工学部研究報告 = Research reports, School of Science and Technology, Meiji University(50):2014.3p.7-13
国立国会図書館全国の図書館
  • 件名Experiment Aerofoil section Pressure measurement ...

Aerodynamics of aerofoil sections measured on a free-flying bird

Aerodynamics of aerofoil sections measured on a free-flying bird
デジタル記事
2010-08-01Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering224 8p.855-864
全国の図書館
  • 要約等...e shape of the aerofoil. The aerodynam......wo-dimensional aerofoil sections were analysed ...... two technical aerofoils, namely the S......23 and Clark Y aerofoils, at 1×10<jats......sup>. The bird aerofoil maintains a robust, near-cons...

Aerodynamic Stall Suppression on Aerofoil Sections Using Passive Air-Jet Vortex Generators

Aerodynamic Stall Suppression on Aerofoil Sections Using Passive Air-Jet Vortex Generators
デジタル記事
2009-09AIAA Journal47 9p.2232-2242
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Design and Analysis of a Controlled Diffusion Aerofoil Section for an Axial Compressor Stator and Effect of Incidence Angle and Mach No. on Performance of CDA

Design and Analysis of a Controlled Diffusion Aerofoil Section for an Axial Compressor Stator and Effect of Incidence Angle and Mach No. on Performance of CDA
デジタル記事
2010International Journal of Fluid Machinery and Systems3 1p.20-28
全国の図書館
  • 要約等...lled Diffusion Aerofoil (CDA) Blade Se......rameters on CD aerofoil at respective ......ure loss on CD aerofoil for the same incidence range ...

Design and Analysis of a Controlled Diffusion Aerofoil Section for an Axial Compressor Stator and Effect of Incidence Angle and Mach No. on Performance of CDA 3 1

Design and Analysis of a Controlled Diffusion Aerofoil Section for an Axial Compressor Stator and Effect of Incidence Angle and Mach No. on Performance of CDA 3 1
デジタル記事
P. Salunke Nilesh, A. Channiwala S.2010International Journal of Fluid Machinery and Systems3 1p.20-28
インターネットで読める全国の図書館
  • 要約等...lled Diffusion Aerofoil (CDA) Blade Se......rameters on CD aerofoil at respective ......ure loss on CD aerofoil for the same incidence range ...

Die shape optimisation in forging of aerofoil sections

Die shape optimisation in forging of aerofoil sections
記事
2003J. Mater. Process. Technol.132p.21-27
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Evaluating the effect of press and die elasticity in forging of aerofoil sections using finite element simulation

Evaluating the effect of press and die elasticity in forging of aerofoil sections using finite element simulation
デジタル記事
2006-06Finite Elements in Analysis and Design42 10p.856-867
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Temperature-related errors on aerofoil section of turbine blade

Temperature-related errors on aerofoil section of turbine blade
記事
2001J. Mater. Process. Technol.115p.240-244
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Preform design for forging of aerofoil sections using FE simulation

Preform design for forging of aerofoil sections using FE simulation
記事
1998Maters. Process. Technol.80p.144-148
全国の図書館

Die-elasticity for precision forging of aerofoil sections using finite element simulation

Die-elasticity for precision forging of aerofoil sections using finite element simulation
記事
1998J. Mater. Process. Technol.76p.56-61
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超音速せん断流中の定常翼形特性

超音速せん断流中の定常翼形特性
紙記事
平野, 公孝, 菊地, 正憲, 川添, 康司, Kawasoe, Yasushi日本機械学会1991-01日本機械学会論文集B編57 533p.153-159
全国の図書館
  • 件名Drag, Supersonic Flow, Shear Flow, Aerofoil, Singularity Method, Lift
  • 並列タイトル等（連結）Steady Characteristics of an Aerofoil Section in a Supersonic Shear...
  • 並列タイトル等Steady Characteristics of an Aerofoil Section in a Supersonic Shear...

Aerodynamic Characteristics of Dragonfly Wing Sections Compared with Technical Aerofoils

Aerodynamic Characteristics of Dragonfly Wing Sections Compared with Technical Aerofoils
デジタル記事
2000-10-15Journal of Experimental Biology203 20p.3125-3135
全国の図書館
  • 要約等...as ultra-light aerofoils which, for st......he ultra-light aerofoils of a dragonfly.</jats:p>

The torsional shearing stress of an aerofoil section. 53 496

The torsional shearing stress of an aerofoil section. 53 496
デジタル記事
齋藤 廣作1987日本機械学会論文集Ａ編53 496p.2400-2405
インターネットで読める全国の図書館
  • 要約等... surface of an aerofoil section was st......ge point of an aerofoil section was lo......surface of the aerofoil section was fo......inertia of the aerofoil section were s......igidity of the aerofoil section was deduced. As an ex...
  • 件名...isson Equation Aerofoil Section Torsional Rigidity Sh...

Aerodynamic characteristics of dragonfly wing sections with technical aerofoils

Aerodynamic characteristics of dragonfly wing sections with technical aerofoils
記事
2000Journal of experimental biology203p.3125-3135
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Aerodynamic Characteristics of Dragonfly Wing Sections Compares with Technical Aerofoils

Aerodynamic Characteristics of Dragonfly Wing Sections Compares with Technical Aerofoils
記事
2000J. Exp. Biol.203p.3125-3135
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Aerodynamic characteristics of dragonfly wing sections compared with technical aerofoils

Aerodynamic characteristics of dragonfly wing sections compared with technical aerofoils
記事
2000J. Exp. Biol.203p.3125-3135
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Aerodynamic Characteristics of Dragonfly Wing Sections Compared with Technical Aerofoils

Aerodynamic Characteristics of Dragonfly Wing Sections Compared with Technical Aerofoils
記事
2000The Journal of Experimental Biology203p.3125-3135
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亜音速せん断流中の定常翼形特性

亜音速せん断流中の定常翼形特性
紙記事
平野, 公孝, 菊地, 正憲, 佐藤, 秀雄, Sato, Hideo日本機械学会1988-11日本機械学会論文集B編54 507p.3175-3180
全国の図書館
  • 件名Subsonic Flow, Shear Flow, Aerofoil, Lift, Singularity Method
  • 並列タイトル等（連結）Steady Characteristics of an Aerofoil Section in a Subsonic Shear F...
  • 並列タイトル等Steady Characteristics of an Aerofoil Section in a Subsonic Shear F...

任意翼型の一部を変更して衝撃波を伴わない翼型を得る解法 26 291

任意翼型の一部を変更して衝撃波を伴わない翼型を得る解法 26 291
デジタル記事
中村 正義1978日本航空宇宙学会誌26 291p.191-198
インターネットで読める全国の図書館
  • 要約等...iven arbitrary aerofoil section can be......tained and the aerofoil section must b......c flows around aerofoil sections which are part......iven arbitrary aerofoil section can be obtained.<BR>A...
  • 並列タイトル等（連結）...nic Flows Past Aerofoil Sections, Partially Mod......iven Arbitrary Aerofoil Section
  • 並列タイトル等...nic Flows Past Aerofoil Sections, Partially Mod......iven Arbitrary Aerofoil Section

Vibration characteristics of pretwisted aerofoil cross-section bladepackets under rotating conditions

Vibration characteristics of pretwisted aerofoil cross-section bladepackets under rotating conditions
デジタル記事
1992-01AIAA Journal30 1p.241-250
全国の図書館