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Flight Handbook, USAF Series C-47/C47A Aircraft , Navy Model R4D-1/R4D-5 Aircraft
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Bibliography of Scientific and Industrial Reports
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A Method for Measuring the Product of Inertia and the Inclination of the Principal Longitudinal Axis of Inertia of an Airplane
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The angle of inclination of the principal axis was found to have probable error of plus or minus 0.17 degrees both from analysis of the error of inertia measure
Technical Note
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Technical Note - National Advisory Committee for Aeronautics
Language: en
Pages: 412
Authors: United States. National Advisory Committee for Aeronautics
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