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A wind-tunnel investigation of the wing loads due to deflected inboard ailerons on a 45 degree sweptback wing at transonic speeds

A. R. Heath, Ann W Igoe

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Abstract

Effects of deflected inboard ailerons on wing loads of 45-deg swept-back wing at transonic speeds

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What this paper is about

Effects of deflected inboard ailerons on wing loads of 45-deg swept-back wing at transonic speeds

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Method / approach

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Main findings

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Available abstract

Effects of deflected inboard ailerons on wing loads of 45-deg swept-back wing at transonic speeds

Key concepts: Aileron, Transonic, Wing, Wind tunnel, Degree (music), Wing configuration, Wing loading, Aerospace engineering

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A wind-tunnel investigation of the wing loads due to deflected inboard ailerons on a 45 degree sweptback wing at transonic speeds — Research Paper | ScholarLens

A wind-tunnel investigation of the wing loads due to deflected inboard ailerons on a 45 degree sweptback wing at transonic speeds

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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