GB/T 14410.2-2008 English PDF

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GB/T 14410.2-2008: Flight mechanics -- Concepts, quantities and symbols -- Part 2: Forces, moments, their coefficients and derivatives
Status: Valid

GB/T 14410.2: Historical versions

Standard ID	USD	BUY PDF	Lead-Days	Standard Title (Description)	Status
GB/T 14410.2-2008	879	Add to Cart	6 days	Flight mechanics -- Concepts, quantities and symbols -- Part 2: Forces, moments, their coefficients and derivatives	Valid
GB/T 14410.2-1993	RFQ	ASK	6 days	Flight mechanics. Concepts, quantities and symbols Forces, moments, their coefficients and derivatives	Obsolete

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GB/T 38905   GB/T 38239   GB/T 36249   GB/T 14410.9   GB/T 14410.8   GB/T 14410.3   

Basic data

Standard ID: GB/T 14410.2-2008 (GB/T14410.2-2008)
Description (Translated English): Flight mechanics -- Concepts, quantities and symbols -- Part 2: Forces, moments, their coefficients and derivatives
Sector / Industry: National Standard (Recommended)
Classification of Chinese Standard: V04
Classification of International Standard: 49.020
Word Count Estimation: 40,494
Date of Issue: 2008-07-18
Date of Implementation: 2009-01-01
Older Standard (superseded by this standard): GB/T 14410.2-1993
Quoted Standard: GB/T 14410.1-2008
Adopted Standard: ISO 1151-3-1989, MOD
Regulation (derived from): National Standard Approval Announcement 2008 No.12 (Total No.125)
Issuing agency(ies): General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China, Standardization Administration of the People's Republic of China
Summary: This standard provides a description of the aircraft movement force, moment coefficients and their derivatives terminology and symbols. This section applies to fixed-wing aircraft. Others may refer to the use of aircraft. The aircraft will be considered as part of a rigid body.

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

---This is a DRAFT version for illustration, not a final translation. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.) will be manually/carefully translated upon your order.
. Flight mechanics Concepts, quantities and symbols Part 2. Forces, moments, their coefficients and derivatives ICS 49.020 Vp 04 National Standards of People's Republic of China Replacing GB/T 14410.2-1993 Flight mechanics - Concepts, quantities and symbols Part 2. Forces, moments, their coefficients and derivatives (ISO 1151-3. 1989, Flightdynamics-Concepts, quantitiesandsymbols- Part 3. Derivativesofforces, momentsandtheircoefficients, MOD) Posted 2008-07-18 2009-01-01 implementation Administration of Quality Supervision, Inspection and Quarantine of People's Republic of China Standardization Administration of China released

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, 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. The main drafters of this section. Wang Lixin, Zhang Shuguang, Shao Arrow, Hong Koon, Quxiang Ju, Jiao Zhiqiang, Li Zhou Fu, Chen Shi Jingsheng, Shaw Yelun, Li Yirui. This part of the standard replaces the previous editions are. --- GB/T 14410.2-1993. Flight mechanics - Concepts, quantities and symbols Part 2. Forces, moments, their coefficients and derivatives

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) α · = Α α · 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) · - = Β · - 3.1.3 dimensionless tangential acceleration normalizedtangentialacceleration Airspeed (GB/T 14410.1-2008 of 3.3.1.2) · - Vp = 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. R (R) ......

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