Norm

ISO 1151-1:1988 en

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

114,67

Over deze norm

Status Definitief
Aantal pagina's 29
Commissie Lucht- en ruimtevaart
Gepubliceerd op 28-04-1988
Taal Engels
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.

Details

ICS-code 01.060
49.020
Nederlandse titel Flight dynamics - Concepts, quantities and symbols - Part 1: Aircraft motion relative to the air
Engelse titel Flight dynamics - Concepts, quantities and symbols - Part 1: Aircraft motion relative to the air

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