Norm

ISO 1151-8:1992 en

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

48,19

Over deze norm

Status Definitief
Aantal pagina's 8
Commissie Lucht- en ruimtevaart
Gepubliceerd op 11-06-1992
Taal Engels
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.

Details

ICS-code 01.060
49.020
Nederlandse titel Flight dynamics - Concepts, quantities and symbols - Part 8: Concepts and quantities used in the study of the dynamic behaviour of the aircraft
Engelse titel Flight dynamics - Concepts, quantities and symbols - Part 8: Concepts and quantities used in the study of the dynamic behaviour of the aircraft

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