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J-GLOBAL ID:202102221421014309   Reference number:21A0255885

Aerodynamic Characteristics of Airfoil with Thin Leading-Edge at Low Reynolds Numbers

低レイノルズ数における薄い前縁を持つ翼型の空力特性
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Volume: 68  Issue:Page: 232-240(J-STAGE)  Publication year: 2020 
JST Material Number: L3565A  ISSN: 1344-6460  Document type: Article
Article type: 原著論文  Country of issue: Japan (JPN)  Language: JAPANESE (JA)
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Aerodynamics of aircrafts 
Reference (20):
  • 1) Schmitz, F. W.: Aerodynamics of the Model Airplane, Part I, Airfoil Measurements, Translation Branch Redstone Scientific Information Center, 1967.
  • 2) Althaus, D.: Profilpolaren für den Modellflug Institut für Aerodynamik und Gasdynamik, University of Stuttgart, 1980.
  • 3) Mueller, T. J.: Aerodynamic Measurements at Low Reynolds Numbers for Fixed Wing Micro-Air Vehicles, Presented at the RTO AVT/VKI Special Course on Development and Operation of UAVs for Military and Civil Applications, 1999.
  • 4) McMasters, J. H. and Henderson, M. L.: Low Speed Single Element Airfoil Synthesis, Tech. Soaring, 2, 2 (1980), pp. 1-21.
  • 5) 大竹智久,中江雄亮,本橋龍郎:低Re数領域でのNACA0012翼の非線形空力特性,日本航空宇宙学会論文集,55 (2007), pp. 439-445.
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