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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| Word Count Estimation | 40,494 | Date of Issue | 2008-07-18 | Date of Implementation | 2009-01-01 | Older Standard (superseded by this standard) | GB/T 14410.2-1993 | Quoted Standard | GB/T 14410.1-2008 | Adopted Standard | ISO 1151-3-1989, MOD | Regulation (derived from) | National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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