Investigation to determine effects of center-of-gravity location on the transonic flutter characteristics of a 45 degree sweptback wing
G. W. Jones, John R. Unangst
Abstract
G. W. Jones, John R. Unangst
Abstract
Report presenting an experimental investigation in the transonic blowdown tunnel to determine effects of center-of-gravity location on the transonic flutter characteristics of a 45 degree sweptback-wing plan form of aspect ratio 4.0 and taper ratio 0.6. Solid-construction models with streamwise NACA 65A004 airfoil sections and center-of-gravity locations at three different chords were fluttered at a range of Mach numbers.
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Report presenting an experimental investigation in the transonic blowdown tunnel to determine effects of center-of-gravity location on the transonic flutter characteristics of a 45 degree sweptback-wing plan form of aspect ratio 4.0 and taper ratio 0.6. Solid-construction models with streamwise NACA 65A004 airfoil sections and center-of-gravity locations at three different chords were fluttered at a range of Mach numbers.
Key concepts: Transonic, Flutter, Airfoil, Center of gravity, Mach number, Wing, Aerodynamics, Degree (music)