Irving R. Abel, Charles L. Ruhlin, Matthew Sanford
Abstract
Wind tunnel flutter analysis of simplified component models of variable-sweep-wing airplane at Mach numbers up to 3
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Wind tunnel flutter analysis of simplified component models of variable-sweep-wing airplane at Mach numbers up to 3
Key concepts: Airplane, Flutter, Wing, Mach number, Component (thermodynamics), Variable (mathematics), Sonic boom, Aeronautics