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GB/T 14410.3-2008 English PDF

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GB/T 14410.3-2008: Flight mechanics -- Concepts, quantities and symbols -- Part 3: Stability and control of aircraft
Status: Valid

GB/T 14410.3: Evolution and historical versions

Standard IDContents [version]USDSTEP2[PDF] delivered inStandard Title (Description)StatusPDF
GB/T 14410.3-2008English439 Add to Cart 4 days [Need to translate] Flight mechanics -- Concepts, quantities and symbols -- Part 3: Stability and control of aircraft Valid GB/T 14410.3-2008
GB/T 14410.3-1993English399 Add to Cart 3 days [Need to translate] Flight mechanics. Concepts, quantities and symbols Stability and control of aircraft Obsolete GB/T 14410.3-1993

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Basic data

Standard ID GB/T 14410.3-2008 (GB/T14410.3-2008)
Description (Translated English) Flight mechanics -- Concepts, quantities and symbols -- Part 3: Stability and control of aircraft
Sector / Industry National Standard (Recommended)
Classification of Chinese Standard V04
Classification of International Standard 49.020
Word Count Estimation 19,193
Date of Issue 2008-07-18
Date of Implementation 2009-01-01
Older Standard (superseded by this standard) GB/T 14410.3-1993
Quoted Standard GB/T 14410.1-2008; GB/T 14410.2-2008; GB/T 14410.6-2008
Adopted Standard ISO 1151-4-1994, 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 specifies the research aircraft stability and control terminology and symbols used (not including the dynamic characteristics). This section applies to fixed-wing aircraft. Can also refer to other aircraft use. Referred to in this section of the body axis system x direction is close to zero lift line of the aircraft.

GB/T 14410.3-2008: Flight mechanics -- Concepts, quantities and symbols -- Part 3: Stability and control of aircraft


---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 3. Stability and control of aircraft ICS 49.020 Vp 04 National Standards of People's Republic of China Replacing GB/T 14410.3-1993 Flight mechanics - Concepts, quantities and symbols Part 3. aircraft stability and control (ISO 1151-4.1994, Flightdynamics-Concepts, quantitiesandsymbols- Part 4. Concepts, quantitiesandsymbolsusedinthestudyofaircraft stabilityandcontrol, 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 3. The partial modification of the use of ISO 1151-4.1994 "Flight dynamics - Concepts, quantities and symbols aircraft stability and control." versus ISO 1151-4.1994 is the main difference. a) ISO 's 4.2.1,4.2.3 merger corresponds to this section 3.1; b) ISO 4.2.2 corresponds to this part 3.3.6,3.3.7; c) ISO 4.2.4,4.3 respectively correspond to the present section 3.4,3.6; d) Added a maneuver point, the neutral point, the maneuver margin, when the static stability grip/release lever margin and other terms. This Part replaces GB/T 14410.3-1993 "Flight mechanics - Concepts, quantities and symbols - Part 3. aircraft stability and control." Section compared with the GB/T 14410.3-1993 The main changes are as follows. a) add stability, controls, volume and other characteristics of the aircraft used for the evaluation to define; b) the original "aerodynamic center" extended to "aerodynamic center and center of pressure"; c) modify the terms and definitions have references to other chapters numbers marked; d) increasing the dimension of the unit, and indicated in the symbols and units columns; e) an increase in the English index. 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. Zhang Shuguang, Hong Koon, Quxiang Ju Shao arrows, Jiao Zhiqiang, Wang Lixin, Zhou Li Fu, Chen, Fan Liqin, Shaw Yelun, Li Yirui. This part of the standard replaces the previous editions are. --- GB/T 14410.3-1993. Flight mechanics - Concepts, quantities and symbols Part 3. aircraft stability and control

1 Scope

This section provides research aircraft stability and control terminology and symbols used (not including the dynamic characteristics). This section applies to fixed-wing aircraft, the aircraft can also refer to other use. X0 directions in this section referred to the body axis system is close to zero lift line aircraft.

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 and units - Part 1. Axis systems and motion state variables GB/T 14410.2-2008 Flight mechanics - Concepts, quantities and symbols and units - Part 2. Forces, moments, their coefficients and derivatives GB/T 14410.6-2008 Flight mechanics - Concepts, quantities and symbols and units - Part 6. Aircraft geometry 3 Terms, definitions and symbols The following terms, definitions and symbols and units apply to this section. No terms are defined or explained symbols and units 3.1.1 Manipulator fixed when Ying Angle aerodynamic center aerodynamiccentre fortheangleofat- tack, motivatorfixed Along the longitudinal axis (GB/T 14410.1-2008 in 3.1.4.1) point P, when the angle of attack (GB/T 14410.1-2008 2.1.2) about changes Aerodynamic pitching moment coefficient of the point (GB/T 14410.2-2008 in 3.3.3.2) (CA m1) P to a constant value, wherein the pitch manipulator (GB/T 14410.1-2008 in 3.6.1) is fixed, that is δ m1 = constant value, CA () m1 P α = 0 3.1.2 Manipulator when loose to float Ying Angle aerodynamic center aerodynamiccentre fortheangleofat- tack, motivatorfree Along the longitudinal axis (GB/T 14410.1-2008 in 3.1.4.1) point P, when the angle of attack (GB/T 14410.1-2008 2.1.2) about changes Aerodynamic pitching moment coefficient of the point (GB/T 14410.2-2008 in 3.3.3.2) (CA m1) P to a constant value, wherein the pitch manipulator (GB/T 14410.1-2008 in 3.6.1) floating loose, ie CA () m1 P α = 0

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