ISO 1151-1:1988

Flight dynamics — Concepts, quantities and symbols — Part 1: Aircraft motion relative to the air

Publication date: 28 pri 1988

General information

Current stage: 90.93 Effective date: 12 jan 2024

Originator: ISO

Owner: ISO/TC 20/SC 8

Type: International Standard

ICS: 49.020 01.060

Gjuha: frëngjisht anglisht

Buying

Statusi: Publikuar

PDF - 17 526 Lekë

Paper - 17 526 Lekë

CD - 17 526 Lekë

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Scope

Gives basic definitions and deals with motion relative to the atmosphere, assumed to be at rest or in translational motion at constant velocity relative to the Earth. The aircraft is assumed to be rigid. However, most of the definitions can be applied to the case of a flexible aircraft. Describes axis systems, angles, velocities and angular velocities, aircraft inertia, forces, moments, coefficients and load factors, thrust, resultant moment of propulsive force, coefficients thereof, control forces and moments, motivators and their forces and moments.

Life cycle

PREVIOUSLY

WITHDRAWN
ISO 1151:1972

WITHDRAWN
ISO 1151-1:1985

NOW

PUBLISHED
ISO 1151-1:1988
90.93 Standard confirmed
12 jan 2024

CORRIGENDA / AMENDMENTS

ABANDON
ISO 1151-1:1988/WD Add 1

REVISED BY

ABANDON
ISO/CD 1151-1

ABANDON
ISO/NP 1151-1