Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20⁰

An edition of Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20⁰ (1984)

Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20

By J. N. Ralston

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Publish Date

1984

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Office,National Technical Information Service]

Language

eng

Pages

Description:

subjects: Mathematical models, Spin (Aerodynamics), Wind tunnel balances