Rotary balance data for a typical single-engine low-wing general aviation design for an angle of attack range 30 ̊to 90 ̊

An edition of Rotary balance data for a typical single-engine low-wing general aviation design for an angle of attack range 30 ̊to 90 ̊ (1978)

Rotary balance data for a typical single-engine low-wing general aviation design for an angle of attack range 30 ̊to 90 ̊

By William Bihrle

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Publish Date

1978

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Office,for sale by the National Technical Information Office

Language

eng

Pages

443

Description:

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