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Effects of modifications to a control surface on a 6-percent-thick unswept wing on the transonic control-surface flutter derivatives

B. J. Gambucci, Robert M Sorenson, John A Wyss

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Abstract

Transonic flutter derivatives for unswept wing control surface configurations determined by pressure cell measurements

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Transonic flutter derivatives for unswept wing control surface configurations determined by pressure cell measurements

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Available abstract

Transonic flutter derivatives for unswept wing control surface configurations determined by pressure cell measurements

Key concepts: Wing, Transonic, Flutter, Flight control surfaces, Surface (topology), Control (management), Aeronautics, Structural engineering

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Effects of modifications to a control surface on a 6-percent-thick unswept wing on the transonic control-surface flutter derivatives — Research Paper | ScholarLens

Effects of modifications to a control surface on a 6-percent-thick unswept wing on the transonic control-surface flutter derivatives

About this research paper

What this paper is about

Why it matters

Key contribution

Method / approach

Main findings

Limitations

Applications

Available abstract

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