ISO 1151-8:1992 PDF
Flight dynamics — Concepts, quantities and symbols — Part 8: Concepts and quantities used in the study of the dynamic behaviour of the aircraft
Open preview (PDF)Flight dynamics — Concepts, quantities and symbols — Part 8: Concepts and quantities used in the study of the dynamic behaviour of the aircraftTitle (English):
ISO 1151-8:1992
Flight dynamics — Concepts, quantities and symbols — Part 8: Concepts and quantities used in the study of the dynamic behaviour of the aircraft
- Document status:
- Withdrawn
- Format:
- Electronic (PDF)
- Number of pages:
- 8
- Publication date:
- June 11, 1992
- Edition:
- ISO IS 1151 edition 1 version 1
- ICS:
- 01.060
Description (English):
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.
Technical details
- Technical committee
- ISO/TC 20/SC 8 - Aerospace terminology
- SKU
- ISO 1151-8:1992
