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Effect of wing loading and altitude on lateral stability and control characteristics of an airplane as determined by tests of a model in the free-flight tunnel

Charles L Seacord

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Abstract

NACA WARTIME REPORTS are reprints of papers originally issued to provide rapid distribution of :1 advance research results to an authorized group requiring them for the war effort.They werepreviously held under a security status but are now unclassified.Some of these reports were not tech-~nically edited.All have been reproduced without change in order to expedite general distribution.

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NACA WARTIME REPORTS are reprints of papers originally issued to provide rapid distribution of :1 advance research results to an authorized group requiring them for the war effort.They werepreviously held under a security status but are now unclassified.Some of these reports were not tech-~nically edited.All have been reproduced without change in order to expedite general distribution.

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OpenAlex reports 1 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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Available abstract

NACA WARTIME REPORTS are reprints of papers originally issued to provide rapid distribution of :1 advance research results to an authorized group requiring them for the war effort.They werepreviously held under a security status but are now unclassified.Some of these reports were not tech-~nically edited.All have been reproduced without change in order to expedite general distribution.

Key concepts: Airplane, Wing, Stability (learning theory), Aircraft flight mechanics, Stability derivatives, Altitude (triangle), Flight control surfaces, Wing loading

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Effect of wing loading and altitude on lateral stability and control characteristics of an airplane as determined by tests of a model in the free-flight tunnel — Research Paper | ScholarLens