Investigation on bomber aircraft to determine overall magnitude of aeroelastic effects on bending and shear strains in rough air show that amplification of strain per unit acceleration in gusts increases with outboard spanwise station to maximum amplification factor of 2.72.
Effects of airplane flexibility on wing strains in rough air at 5,000 feet as determined by flight tests of large swept-wing airplane
NACA -- Tech Note
NACA -- Technical Note ; n 4107
1957
32 pages
Article (Journal)
English
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