ISO 1151-1:1988

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

OVERVIEW

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.

COMMENTS

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PRODUCT DETAILS

Status Current
Edition 1988
No. of Pages 29
ICS Classification 01.060 Quantities and units
49.020 Aircraft and space vehicles in general
Committee ISO/TC 20/SC 8
Available for Purchase For sale in Singapore only
Adoption ISO