ISO-1151-8 Historical Revision Information
Flight dynamics - Concepts, quantities and symbols - Part 8: Concepts and quantities used in the study of the dynamic behaviour of the aircraft

ISO-1151-8 - 1ST EDITION - SUPERSEDED
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The aircraft is assumed to be rigid, of constant mass and of constant inertia. It is not equipped with systems modifying its natural dynamic behaviour. However, most of the definitions can be applied to the case of a flexible aircraft, of variable mass and of variable inertia. The general concepts defined are applicable to the atmospheric flight phase.

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Document Number

ISO 1151-8:1992

Revision Level

1ST EDITION

Status

Superseded

Publication Date

June 15, 1992

Committee Number

ISO TC 20/SC 3