Superseded , Reaffirmed Standard
Historical

ISO 1151-8:1992 (R2018)

Flight dynamics — Concepts, quantities and symbols
Part 8: Concepts and quantities used in the study of the dynamic behaviour of the aircraft

Summary

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.

Notes

95.99 : Annulation de la Norme internationale

Technical characteristics

Publisher International Organization for Standardization (ISO)
Publication Date 06/11/1992
Confirmation Date 12/17/2018
Edition 1
Page Count 8
EAN ---
ISBN ---
Weight (in grams) ---
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