Low reynolds number airfoil performance subjected to wake interference from an upstream airfoil

5th Applied Aerodynamics Conference, 1987

Volumn , Issue , 1987, Pages

  Michelsen, W D ^a   Mueller, T J ^a  

^a UNIVERSITY OF NOTRE DAME   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; FLOW VELOCITY; REYNOLDS NUMBER; STRAIN GAGES; WAKES; WIND TUNNELS;

AERODYNAMIC COEFFICIENTS; LOW REYNOLDS NUMBER; LOW REYNOLDS NUMBER AIRFOILS; PERFORMANCE DATA; PERFORMANCE MEASUREMENTS; SEPARATION DISTANCES; VELOCITY DEFICITS; WAKE INTERFERENCES;

AIRFOILS;

EID: 85002205120     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1987-2351     Document Type: Conference Paper

References (5)

1. Young, A.D, Morris, D.E., “Note on Flight Tests on the Effect of Slipstream on Boundary- Layer Flow,” R&M No. 1957, Brit. A.R.C., 1939.
2. Hood, M.J. and Gaydos, M.E., “Effects of Propellers and Vibration on the Extent of Laminar Flow on the NACA 27-212 Airfoil,” NACA ACR (WR L-784), 1939.
3. 6, International Conference, Royal Aeronautical Society, London, October 1986.
4. Michelsen, Wayne D., “The Effects of Upstream Wake Interference on the Performance of a Low Reynolds Number Airfoil in a Two-Dimensional Canard/Wing Configuration.” Masters Thesis, University of Notre Dame, 1987.
5. Hoerner, Sighard F., and Borst, Henry V., “Lift of Aiplane Configurations,” Chapter XX, pp.20-12, Fluid Dynamic Lift, publisher: Mrs. Liselotte A. Hoerner, 1975