Theory of divergence of constant thickness rectangular plate wings is presented, based on assumptions of linear elastic theory and linearized aerodynamic theory; critical conditions occurred at M equal 1; it is established that sweeping leading edge of plate airfoil of constant thickness increases its stability; divergence conditions.
Divergence of plate airfoils of low aspect ratio at supersonic speeds
J Aero/Space Sciences
Journal of the Aero/Space Sciences ; 26 , n 8
1959
Aufsatz (Zeitschrift)
Englisch
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