27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS 2010-2.10.1

DESIGN AND WIND TUNNEL TESTING OF CAL POLY’S AMELIA 10 FOOT SPAN HYBRID WING-BODY LOW NOISE CESTOL AIRCRAFT

K. K. Jameson, D. D. Marshall, R. Ehrmann, E. Pacino, R. Golden, D. Mason*
California Polytechnic State Univ., USA; *PatersonLabs, USA

Keywords: powered-lift, circulation control, cfd database, nfac

California Polytechnic Corporation with GTRI and DHC Engineering worked on a NASA NRA to develop and validate predictive capabilities for the design and performance of CESTOL low noise subsonic aircraft including a 1/12 scale model and wind tunnel test in a 40' by 80' wind tunnel.

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