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ISO 1151-1:1988-ed.4.0
Flight dynamics — Concepts, quantities and symbols — Part 1: Aircraft motion relative to the air
Automatically translated name:
Flight dynamics -- Concepts, quantities and symbols -- Part 1: Aircraft motion relative to the air
STANDARD published on 28.4.1988
The information about the standard:
Designation standards: ISO 1151-1:1988-ed.4.0
Publication date standards: 28.4.1988
SKU: NS-423230
The number of pages: 29
Approximate weight : 87 g (0.19 lbs)
Country: International technical standard
Category: Technical standards ISO
The category - similar standards:
Annotation of standard text ISO 1151-1:1988-ed.4.0 :
Description / 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.
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