Characteristics of wings of high aspect ratio experiencing bending and torsional deformations, calculated for supersonic speed by application of linearized lifting surface theory; calculations for wing of aspect ratio 3.2 and 60° sweepback are presented for Mach number 1.414 and for incompressible flow.
Longitudinal stability of elastic swept wings at supersonic speed
Nat Advisory Committee Aeronautics -- Tech Note
1949
38 pages
Report
English
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Longitudinal stability of elastic swept wings at supersonic speed
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