Art

J-GLOBAL ID：201202272098866431   Reference number：12A1639624

CFD-Aided Evaluation of Reynolds Number Scaling Effect Accounting for Static Model Deformation

静的モデル変形を考慮したReynolds数スケーリング効果のCFD援用評価

Author (2)： YASUE Kanako (Dep. of Aerospace Engineering, Tohoku Univ.) ,  SAWADA Keisuke (Dep. of Aerospace Engineering, Tohoku Univ.)
Material： Transactions of the Japan Society for Aeronautical and Space Sciences  (Trans Jpn Soc Aeronaut Space Sci)
Volume： 55  Issue： 5  Page： 321-331 (J-STAGE)  Publication year： 2012 
JST Material Number： F0167A  ISSN： 0549-3811  CODEN： TJASA  Document type： Article
Article type： 原著論文  Country of issue： Japan (JPN)  Language： ENGLISH (EN)

Thesaurus term： scaling ,  *Reynolds number ,  *aeroelasticity ,  *transonic flow ,  Galerkin method ,  wing tip ,  wind tunnel test ,  bending (material phenomenon) ,  angle of attack ,  sweptback wing ,  deformation ,  lift coefficient ,  reduction ,  computational fluid dynamics ,  drag reducing ,  fluid dynamics ,  Physics ,  Science ,  Mechanics ,  continuum mechanics ,  natural science
Semi thesaurus term： computational fluid dynamics ,  method of structural analysis ,  drag reduction

JST classification (1)： Flying object design and structure  (QK04010H)

Reference (17)：

• BUSHNELL, D. M. Scaling : Wind Tunnel to Flight. Annu. Rev. Fluid Mech. 2006, 38, 111-128
• MCKINNEY, L. W. National Transonic Facility Status. 1989
• National Transonic Facility. http://www.aeronautics.nasa.gov/atp/facilities/ntf/index.html
• KILGORE, W. A. Recent Enhancements to the National Transonic Facility. 2003
• QUEST, J. ETW-High Quality Test Performance in Cryogenic Environment. 2000

Terms in the title (5)： モデル ,  Reynolds数 ,  スケーリング ,  援用 ,  評価