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STATIC STABILITY AND CONTROL CHARACTERISTICS OF AN AIRPLANE MODEL WITH TAIL SURFACES OUTBOARD OF THE WING TIPS AT A MACH NUMBER OF 2.01

Cornelius Driver, M Leroy Spearman

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Abstract

Static stability and control characteristics of aircraft model with tail surfaces outboard of wing tips

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Static stability and control characteristics of aircraft model with tail surfaces outboard of wing tips

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Available abstract

Static stability and control characteristics of aircraft model with tail surfaces outboard of wing tips

Key concepts: Airplane, Wing, Longitudinal static stability, Mach number, Flight control surfaces, Stability (learning theory), Aerospace engineering, Wing configuration

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STATIC STABILITY AND CONTROL CHARACTERISTICS OF AN AIRPLANE MODEL WITH TAIL SURFACES OUTBOARD OF THE WING TIPS AT A MACH NUMBER OF 2.01 — Research Paper | ScholarLens

STATIC STABILITY AND CONTROL CHARACTERISTICS OF AN AIRPLANE MODEL WITH TAIL SURFACES OUTBOARD OF THE WING TIPS AT A MACH NUMBER OF 2.01

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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