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Estimates of the vertical-tail loads of a Bell P-63A-1 airplane (AAF No. 42-68889) in accelerated rolling maneuvers based on flight tests with two vertical-tail arrangements

Harold I Johnson

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Abstract

NACA WARTIME REPORTS are reprints of papers originally issued tu provide r apid distribution of advance research results to an authorized group requiring t em for the war effort.They 'Were previously held under a security status but are now unclassiiled.Some of these reports were not technically 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 tu provide r apid distribution of advance research results to an authorized group requiring t em for the war effort.They 'Were previously held under a security status but are now unclassiiled.Some of these reports were not technically edited.All have been reproduced without change in order to expedite general distribution.

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OpenAlex reports 2 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 tu provide r apid distribution of advance research results to an authorized group requiring t em for the war effort.They 'Were previously held under a security status but are now unclassiiled.Some of these reports were not technically edited.All have been reproduced without change in order to expedite general distribution.

Key concepts: Airplane, Acceleration, Longitudinal static stability, Mathematics, Physics, Engineering, Mechanics, Aerospace engineering

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Estimates of the vertical-tail loads of a Bell P-63A-1 airplane (AAF No. 42-68889) in accelerated rolling maneuvers based on flight tests with two vertical-tail arrangements — Research Paper | ScholarLens