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WIND-TUNNEL INVESTIGATION OF DEVICES TO IMPROVE STATIC DIRECTIONAL STABILITY OF AN UNSWEPT-WING AIRPLANE MODEL AT MACH NUMBERS FROM 0.8 TO 2.2

Ralph W Holtzclaw

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Abstract

Wind tunnel tests to improve static directional stability of unswept-wing aircraft at mach 0.8-2.2

About this research paper

What this paper is about

Wind tunnel tests to improve static directional stability of unswept-wing aircraft at mach 0.8-2.2

Why it matters

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Key contribution

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Method / approach

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Main findings

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Available abstract

Wind tunnel tests to improve static directional stability of unswept-wing aircraft at mach 0.8-2.2

Key concepts: Airplane, Wing, Wind tunnel, Mach number, Longitudinal static stability, Aeronautics, Aerospace engineering, Stability (learning theory)

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WIND-TUNNEL INVESTIGATION OF DEVICES TO IMPROVE STATIC DIRECTIONAL STABILITY OF AN UNSWEPT-WING AIRPLANE MODEL AT MACH NUMBERS FROM 0.8 TO 2.2 — Research Paper | ScholarLens