Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8 ̊to 90 ̊
An edition of Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8 ̊to 90 ̊ (1978)
By William Bihrle
Publish Date
1978
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office,for sale by the National Technical Information Service
Language
eng
Pages
464
Description:
subjects: Reynolds number, Airplanes, Wings, Spin (Aerodynamics)