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Wind-tunnel investigation of the OMAC canard configuration (1986)

Ingram, W. C. ; Yip, L. P. ; Cook, E. L.

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Publication Date: 2019-06-28

Description: Wind-tunnel tests were conducted on a 0.175-scale model of the OMAC Laser 300 canard configuration in the NASA Langley 12-Foot Low-Speed Wind Tunnel to determine its low-speed high angel-of-attack aerodynamic characteristics. The Laser 300 is a general aviation turboprop pusher aircraft utilizing a canard configuration. The design incorporates a low forward wing and a high main wing with a leading-edge droop installed on the outboard panel and tip fins mounted on the wing tips. The model was tested over a range of -6 to 50-deg angle-of-attack and 20 to -20 deg sideslip. Static force and moment data were measured, and the longitudinal and lateral-directional characteristics were determined.

Keywords: AERODYNAMICS

Type: AIAA PAPER 86-2608

Format: text

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