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Calculation of flutter characteristics for finite-span swept or unswept wings at subsonic and supersonic speeds by a modified strip analysis

E. Carson Yates

Abstract

Report presenting a method for calculating flutter characteristics of finite-span swept or unswept wings at subsonic and supersonic speeds. Flutter characteristics were calculated using this method for 12 wings of varying sweep angle, aspect ratio, taper ratio, and center-of-gravity position at a range of Mach numbers.

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Available abstract

Key concepts: Flutter, Supersonic speed, Span (engineering), Mach number, Position (finance), Structural engineering, Swept wing, Range (aeronautics)