27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS 2010-6.10.1

EXPERIMENTAL AND COMPUTATIONAL STUDY OF TWO FLAPPED AIRFOILS AT LOW REYNOLDS NUMBERS
N. Ylilammi, A. V. G. Cavalieri*, G. Soinne
Aalto Univ. School of Science and Technology, Finland; *ITA, Brazil
Keywords: airfoil, cfd, experiment, low reynolds number

Two airfoils, NACA 2412 and SD 7062 with plain flaps, were tested experimentally at a low Reynolds number range typical for UAVs. The results were compared with a handbook method and computations with two CFD codes.

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27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS 2010-6.10.1

EXPERIMENTAL AND COMPUTATIONAL STUDY OF TWO FLAPPED AIRFOILS AT LOW REYNOLDS NUMBERS

N. Ylilammi, A. V. G. Cavalieri, G. Soinne
Aalto Univ. School of Science and Technology, Finland; ITA, Brazil

Keywords: airfoil, cfd, experiment, low reynolds number

Two airfoils, NACA 2412 and SD 7062 with plain flaps, were tested experimentally at a low Reynolds number range typical for UAVs. The results were compared with a handbook method and computations with two CFD codes.

view full paper

27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France Paper ICAS 2010-6.10.1

EXPERIMENTAL AND COMPUTATIONAL STUDY OF TWO FLAPPED AIRFOILS AT LOW REYNOLDS NUMBERS

N. Ylilammi, A. V. G. Cavalieri*, G. Soinne Aalto Univ. School of Science and Technology, Finland; *ITA, Brazil

Keywords: airfoil, cfd, experiment, low reynolds number Two airfoils, NACA 2412 and SD 7062 with plain flaps, were tested experimentally at a low Reynolds number range typical for UAVs. The results were compared with a handbook method and computations with two CFD codes.

view full paper

27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS 2010-6.10.1

N. Ylilammi, A. V. G. Cavalieri, G. Soinne
Aalto Univ. School of Science and Technology, Finland; ITA, Brazil

Keywords: airfoil, cfd, experiment, low reynolds number

Two airfoils, NACA 2412 and SD 7062 with plain flaps, were tested experimentally at a low Reynolds number range typical for UAVs. The results were compared with a handbook method and computations with two CFD codes.