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 View on Open Library

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

by E. Richard White

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First published: 1982 1 language
Subjects
Spin (Aerodynamics) Leading edges (Aerodynamics) Stalling (Aerodynamics)

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