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GB/T 14410.2-2008Flight mechanics -- Concepts, quantities and symbols -- Part 2: Forces, moments, their coefficients and derivatives (English PDF)

飞行力学 概念、量和符号 第2部分:力、力矩及其系数和导数

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Issued by

Standardization Administration of China

Level / Type

National · Recommended

Issue date

July 18, 2008

Implementation date

January 1, 2009

Scope

GB/T 14410.2-2008 is the English-translated version of 飞行力学 概念、量和符号 第2部分:力、力矩及其系数和导数.

GB/T 14410.2-2008 — This section provides a description of the aircraft movement forces, moments, their coefficients and derivatives of terminology and symbols.

This section applies to fixed-wing aircraft, other aircraft can use the reference. The aircraft will be considered as part of a rigid body.

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Document preview — GB/T 14410.2-2008

National Standard of the People's Republic of China

ICS
49.020
Classification
V 04
Replacing
GB/T 14410.2-1993

Issued by: Standardization Administration of China

Contents

  • Foreword
  • 1 Scope
  • 2 Normative references
  • 3 Terms, definitions and symbols

Foreword

GB/T 14410 "Flight mechanics - Concepts, quantities and symbols" is divided into nine sections.

--- Part 1. Axis systems and motion state variables;

--- Part 2. Forces, moments, their coefficients and derivative;

--- Part 3. aircraft stability and control;

--- Part 4. flight performance;

--- Part 5. flight measurement;

--- Part 6. Aircraft geometry;

--- Part 7. Flight points and flight envelope;

--- Part 8. dynamic characteristics of the aircraft;

--- Part 9. atmospheric disturbance model.

This section GB/T 14410 Part 2.

The partial modification of the use of ISO 1151-3. 1989 (E) "Flight dynamics - Concepts, quantities and symbols - Part 3. forces, moments and lines Number and Derivatives. " This standard and ISO 1151-3. 1989 as compared to a major increase "dimensionless angle of attack, sideslip angle and airspeed derivative with respect to time, up Lower rudder hinge moment pneumatic, aileron hinge moment "and other terms.

This Part replaces GB/T 14410.2-1993 "Flight mechanics - Concepts, quantities and symbols - Part 2. Forces, moments, their coefficients and Derivative".

Section compared with the GB/T 14410.2-1993 The main changes are as follows.

a) an increase of more than force than the force component than the combined torque than the combined torque components, directly derivative than derivatives are estimated definitions;

b) the symbol M Mach modify M Rao, the term "dimensionless" to "dimension", "vector" to "Vector";

c) modify the terms and definitions have a number of references to other clauses marked;

d) increasing the dimension of the unit, and indicated in the symbol bar;

e) an increase in the English index.

Appendix A to this part of the normative appendix.

This part is proposed by the China Aviation Industry Corporation.

This part of the jurisdiction of the China Aviation Industry Corporation.

This section is drafted. Beijing University of Aeronautics and Astronautics, China Aviation Technology Institute Comprehensive, China Aviation Industry Research Institute of air power, in State Aviation Industry Development Research Center.

1 Scope

This section provides a description of the aircraft movement forces, moments, their coefficients and derivatives of terminology and symbols.

This section applies to fixed-wing aircraft, other aircraft can use the reference.

The aircraft will be considered as part of a rigid body.

2 Normative references

The following documents contain provisions which, through reference in this text, constitute provisions of this part. For dated references, subsequent Amendments (not including errata content) or revisions do not apply to this section, however, encourage the parties to this part of the research agreement Whether the latest versions of these documents. For undated reference documents, the latest versions apply to this section.

GB/T 14410.1-2008 Flight mechanics - Concepts, quantities and symbols - Part 1. Axis systems and motion state variables

3 Terms, definitions and symbols

The following terms, definitions and symbols apply to this section.

No terms are defined or explained symbols and units

3.1.1 Dimensionless rate of change of angle of attack

normalizedrateofchangeofthe angleofattack Angle of attack (GB/T 14410.1-2008 of 3.2.1.2) alpha · = Alpha alpha ·

3.1.2 Dimensionless rate of change of angle of sideslip

normalizedrateofchangeofthe angleofsideslip Slip angle (GB/T 14410.1-2008 of 3.2.1.1)

= Beta

3.1.3 Dimensionless tangential acceleration

normalizedtangentialacceleration Airspeed (GB/T 14410.1-2008 of 3.3.1.2)

Vp 2

No terms are defined or explained symbols and units

3.2.1 Force

resultantforce

The force acting on the aircraft such force vector. include Thrust and aerodynamic body, but does not include gravity, inertia Reaction force and ground contact.

......
This preview omits tables, figures, formulas and parts of the technical clauses. The complete document — 23 pages — is available in the English PDF.

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