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Flight dynamics — Concepts, quantities and symbols — Part 3: Derivatives of forces, moments and their coefficients
Automatically translated name:
Flight dynamics -- Concepts, quantities and symbols -- Part 3: Derivatives of forces, moments and their coefficients
STANDARD published on 6.4.1989
Designation standards: ISO 1151-3:1989-ed.2.0
Publication date standards: 6.4.1989
SKU: NS-423234
The number of pages: 10
Approximate weight : 30 g (0.07 lbs)
Country: International technical standard
Category: Technical standards ISO
Description / Abstract: Deals with derivatives of forces, moments and of other quantities characterizing such forces and moments. The term "derivative" designates the partial derivative of a function with respect to an independent variable. These derivatives appear in the terms of the Taylor series representing the variations of functions with the independent variables. Is restricted to first-order terms. Terms of higher order would require additional definitions of higher order. The aircraft is assumed to be rigid. However, most of the definitions can be applied to the case of a flexible aircraft.
Flight dynamics — Concepts, quantities and symbols — Part 3: Derivatives of forces, moments and their coefficients — Technical Corrigendum 1
(Mécanique du vol — Concepts, grandeurs et symboles — Partie 3: Dérivées des forces, des moments et de leurs coefficients — Rectificatif technique 1)
Correction published on 7.3.1996
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