ISO 1151-1:1988
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ISO 1151-1:1988
5699

Status : Published (Under review)

This standard was last reviewed and confirmed in 2024. Therefore this version remains current.
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Format Language
std 1 151 PDF
std 2 151 Paper
  • CHF151
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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.

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General information

  •  : Published
     : 1988-04
    : International Standard confirmed [90.93]
  •  : 4
     : 29
  • ISO/TC 20/SC 8
    01.060  49.020 
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Life cycle

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