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About this nonfiction

Wind-tunnel investigation at high subsonic speeds of the effect of spoiler profile on the lateral control characteristics of a wing-fuselage combination winter quarter-chord line swept back 32.6° and NACA 65A006 airfoil section by Johnson, Harold S. is a nonfiction available to read on EtoBox.

It is typically read by self-directed learners exploring a subject in depth.

Common subject areas: history, science, philosophy, social sciences.

Author
Johnson, Harold S.
Publisher
National Advisory Committee for Aeronautics, 1953.
Published
1953
Language
EN
Category
nonfiction

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