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GB/T 14410.6-2008 English PDF

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GB/T 14410.6-2008: Flight mechanics -- Concepts, quantities and symbols -- Part 6: Aircraft geometry
Status: Valid

GB/T 14410.6: Evolution and historical versions

Standard IDContents [version]USDSTEP2[PDF] delivered inStandard Title (Description)StatusPDF
GB/T 14410.6-2008English529 Add to Cart 4 days [Need to translate] Flight mechanics -- Concepts, quantities and symbols -- Part 6: Aircraft geometry Valid GB/T 14410.6-2008
GB/T 14410.6-1993English639 Add to Cart 5 days [Need to translate] Flight mechanics. Concepts, quantities and symbols Aircraft geometry Obsolete GB/T 14410.6-1993

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Basic data

Standard ID GB/T 14410.6-2008 (GB/T14410.6-2008)
Description (Translated English) Flight mechanics -- Concepts, quantities and symbols -- Part 6: Aircraft geometry
Sector / Industry National Standard (Recommended)
Classification of Chinese Standard V04
Classification of International Standard 49.020
Word Count Estimation 23,244
Date of Issue 2008-07-18
Date of Implementation 2009-01-01
Older Standard (superseded by this standard) GB/T 14410.6-1993
Quoted Standard GB/T 14410.1-2008
Adopted Standard ISO 1151-6-1982/Amd.1-1984, 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 flight mechanics and related, basic terminology and symbols used to describe the geometry of the aircraft, these terms and symbols are not described in detail the shape of the aircraft completely. This section applies to fixed-wing aircraft. Others may refer to the use of aircraft.

GB/T 14410.6-2008: Flight mechanics -- Concepts, quantities and symbols -- Part 6: Aircraft geometry


---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 6. Aircraft geometry ICS 49.020 Vp 04 National Standards of People's Republic of China Replacing GB/T 14410.6-1993 Flight mechanics - Concepts, quantities and symbols Part 6. Aircraft geometry (ISO 1151-6. 1982/Amd1. 1984Termsandsymbolsforflightdynamics- Part 6. Aircraftgeometry, 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 6. The partial modification of the use of ISO 1151-6. 1982/Amd1. 1984 "aircraft flight dynamics geometry terminology and symbols." this Part of ISO 1151-6. 1982/Amd1. 1984 The main difference is the addition of "shafting aircraft structure, the trailing arm horizontal tail, vertical tail Trailing arm "and other terms. This Part replaces GB/T 14410.6-1993 "Flight mechanics - Concepts, quantities and symbols - Part 6. Aircraft geometry." Section compared with the GB/T 14410.6-1993 The main changes are as follows. a) increase the "reference axis components 3.1.6", "3.5.8 center chord length" and other terms and definitions; b) Modify the "3.5.11 wing trapezoid ratio" is "3.5.12 aircraft wingtip root ratio" and other definitions; 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. 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. Quxiang Ju, Wang Lixin, Hong Koon, Jiao Zhiqiang, Zhang Shuguang, Shao arrows, Chen, Zhou Li Fu, Yu Duixin, Shaw Yelun, Li Yirui. This part of the standard replaces the previous editions are. --- GB/T 14410.6-1993. Flight mechanics - Concepts, quantities and symbols Part 6. Aircraft geometry

1 Scope

This section provides relevant and flight mechanics, aircraft used to describe the geometry of the basic terminology and symbols, these terms and symbols And not described in detail the shape of the aircraft completely. This section applies to fixed-wing aircraft, other aircraft can use the reference.

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 Aircraft reference plane aircraftreferenceplane The main parts of the aircraft relative to this surface is the left and right of Said arrangement. The reference plane is the plane shaft (3.1.4) The R z R x0 surface. NOTE. In most cases, the aircraft fuselage reference plane and a reference Face is the same. Z R R x0 3.1.2 Airplane reference point aircraftreferencepoint Aircraft reference surface (3.1.1) on a suitably chosen Points. OR 3.1.3 Aircraft reference axis aircraftreferenceaxis By airplane reference point (3.1.2) and the forward direction, solid Aircraft scheduled to reference plane in a straight line (3.1.1) on. X0 R 3.1.4 Airplane reference shaft aircraftreferenceaxissystem Fixed to the shaft on the plane, the origin of the reference plane Point (3.1.2), the R-axis x0 aircraft reference axis (3.1.3) Consistent, right y axis R, R z axis is the reference surface of the aircraft (3.1.1), the downward direction. NOTE. In most cases, the aircraft fuselage reference shaft and the shaft System (3.4.1) is the same. OR x0 R y R z R 3.1.5 Part reference point referencepointofacomponent On the part suitably selected fixed point. 3.1.6 Member reference axis Referenceaxisofacomponent Fixedly connected to the member by member reference point (3.1.5) In the appropriate direction in a straight line.

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