23rd Congress of International Council of the Aeronautical Sciences, 8-13 September, 2002, Toronto, Canada
Paper ICAS 2002-3.8.3

AERODYNAMIC CHARACTERISTICS OF SPIN PHENOMENON FOR DELTA WING

Y. Nakamura, T. Yamada
Nagoya University, Japan

Keywords: Null

The experiments of delta wing spinning phenomenon were conducted at the low speed wind tunnel of Nagoya University, whose exit was turned upward. The spin rate of the delta wing in the free rotation mode was measured as well as surface pressure distributions on the spinning delta wing.

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