Characteristics of rotary wings in hovering mode at an ultra-low reynolds number

Transactions of the Japan Society for Aeronautical and Space Sciences

Volumn 47, Issue 155, 2004, Pages 59-65

  Sunada, Shigeru ^a   Ohkura, Akihiro ^a   Matsue, Atsushi ^a   Kawachi, Keiji ^b  

^a Osaka Prefecture University   (Japan)

^b UNIVERSITY OF TOKYO   (Japan)

Author keywords

Annular Momentum Theory; Blade Element Theory; Rotary Wing; Ultra Low Reynolds Number

Indexed keywords

AERODYNAMICS; ASPECT RATIO; ESTIMATION; MEASUREMENT THEORY; REYNOLDS NUMBER;

ANNULAR MOMENTUM THEORY; BLADE ELEMENT THEORY; ROTARY WING; ULTRA-LOW REYNOLDS NUMBER;

WINGS;

EID: 33747629134     PISSN: 05493811     EISSN: 05493811     Source Type: Journal    
DOI: 10.2322/tjsass.47.59     Document Type: Article

References (5)

1. Gessow, A. and Myers, G. C: Aerodynamics of the Helicopter, College Park Press, Maryland, 1967.
2. Sunada, S., Yasuda, T., Yasuda, K. and Kawachi, K.: Comparison of Wing Characteristics at a Low Reynolds Number, J. Aircraft, 39 (2002), pp. 331-338.
3. Sunada, S. and Kawachi, K.: Effects of Reynolds Number on Characteristics of Fixed and Rotary Wings, J. Aircraft, 41 (2004), pp. 189-192.
4. Usherwood, J. R. and Ellington, C. P.: The Aerodynamics of Revolving Wings. I. Model Hawkmoth Wings, J. Exp. Biol., 205 (2002), pp. 1547-1564.
5. Abbott, I. H. and Von Doenhoff, A. E.: Theory of Wing Section, Dover, New York, 1949.