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Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft
E. Richard White1982
Spin-tunnel investigation of the spinning characteristics of typical single-engine general aviation airplane designs
Sanger M. Burk1977
Spin-tunnel investigation of a 1/13-scale model of the NASA AD-1 oblique-wing research aircraft
William L White1982
Rotary balance data for a single-engine general aviation design having a high aspect-ratio canard for an angle-of-attack range of 30 ̊to 90 ̊
William Mulcay1980