ISO 1151-1:1988

Status : Published (Under review)

This standard was last reviewed and confirmed in 2018. Therefore this version remains current.

	Format	Language
std 1 145	PDF
std 2 145	Paper

CHF145

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Abstract

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.

General information

Status
: Published

Publication date
: 1988-04

Stage
: International Standard under systematic review [90.20]
Edition
: 4

Number of pages
: 29
Technical Committee :
ISO/TC 20/SC 8

ICS :
01.060 49.020
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