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

Abstract

 Preview

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 

  •  :  Published
     : 1988-04
  •  : 4
     : 29
  •  : ISO/TC 20/SC 8 Aerospace terminology
  •  :
    01.060 Quantities and units
    49.020 Aircraft and space vehicles in general

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std 1 138 PDF
std 2 138 Paper
  • CHF138

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