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NACA-TR-711

Analysis and prediction of longitudinal stability of airplanes

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1941

Abstract: An analysis has been made of the longitudinal stability characteristics of 15 airplanes as determined in flight. In the correlation of satisfactory and unsatisfactory characteristics with determined values, the derivative that expresses the ratio of static-restoring moments to elevator-control moments was found to represent most nearly the stability characteristics appreciated by the pilots. The analysis was extended to study the effects of various design features on the observed stability characteristics. Design charts and data are included that show the effects on longitudinal stability of relative positions of wing and tail, fuselage size and location, engine nacelles, and horizontal-tail arrangements.
URI: https://yse.yabesh.ir/std/handle/yse/20558
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    NACA-TR-711

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:20:37Z
date available2017-09-04T15:20:37Z
date copyright01/01/1941
date issued1941
identifier otherMWWUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/20558
description abstractAn analysis has been made of the longitudinal stability characteristics of 15 airplanes as determined in flight. In the correlation of satisfactory and unsatisfactory characteristics with determined values, the derivative that expresses the ratio of static-restoring moments to elevator-control moments was found to represent most nearly the stability characteristics appreciated by the pilots. The analysis was extended to study the effects of various design features on the observed stability characteristics. Design charts and data are included that show the effects on longitudinal stability of relative positions of wing and tail, fuselage size and location, engine nacelles, and horizontal-tail arrangements.
languageEnglish
titleNACA-TR-711num
titleAnalysis and prediction of longitudinal stability of airplanesen
typestandard
page10
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1941
contenttypefulltext
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