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AIR1678B
Uncertainty of In-Flight Thrust Determination
Uncertainty of In-Flight Thrust Determination
2011-05-01
有效
【范围】 This document defines and illustrates the process for determination of uncertainty of turbofan and turbojet engine in-flight thrust and other measured in-flight performance parameters. The reasons for requiring this information, as specified in the E-33 Charter, are: determination of high confidence aircraft drag; problem rectification if performance is low; interpolation of measured thrust and aircraft drag over a range of flight conditions by validation and development of high confidence analytical methods; establishment of a baseline for future engine modifications. This document describes systematic and random measurement uncertainties and methods for propagating the uncertainties to the more complicated parameter, in-flight thrust. Methods for combining the uncertainties to obtain given confidence levels are also addressed. Although the primary focus of the document is in-flight thrust, the statistical methods described are applicable to any measurement process. The E-33 Committee has endeavoured to gather industry-wide expertise in in-flight measurement and uncertainty analysis to collect and promulgate recommended practices in the subject disciplines. The Committee is organized into subcommittees to address both the analytical and test methodology for determination of in-flight thrust and also the uncertainty of the determination. This document; Uncertainty of In-flight Thrust Determination, AIR1678, addresses the process for determining the uncertainty of in-flight thrust. A companion document, In-Flight Thrust Determination, AIR1703, addresses the basic methodology for determining in-flight thrust. The Committee, after reviewing recommended changes and clarification in definitions and application of statistical uncertainty items, made small revisions to the original document published in 1985. These changes were incorporated into AIR1678 Rev A. This Revision B has the same Scope as preceding versions. The nomenclature and methodology used herein are now consistent with evolving world and national standards promulgated primarily by ISO and ASME.strRefField
【与前一版的变化】

替代标准

引用文件/被引文件

In-Flight Thrust Determination
Application of In-Flight Thrust Determination Uncertainty
(Revision of ASME PTC 19.1-1998)
Quality Assurance requirements for measuring equipment - Part 1: Metrological confirmation system for measuring equipment.
Guide to the Expression of Uncertainty in Measurement.
Improvement of Parameter Estimation Through Uncertainty Analysis

包含图表

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MEASUREMENT ERROR, δ
ERROR CLASSIFICATION
MEASUREMENT ERROR CO
NORMAL DISTRIBUTION
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SYSTEMATIC ERROR
MEASUREMENT CALIBRAT
CALIBRATION HIERARCH
TEST ARTICLE AND / O
EXAMPLE DATA ACQUISI
TYPICAL DATA ACQUISI
TYPICAL DATA REDUCTI
TYPICAL ERRORS OF ME
DISTRIBUTION OFiX AN
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SYSTEMATIC STANDARD
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RECOMMENDED TABLE FO
RECOMMENDED TABLE FO
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FIGURE 11 - GROUND T
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GENERAL FLIGHT TEST
IN-FLIGHT THRUST MEA
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EXAMPLE PRELIMINARY
GROUND TEST MEASUREM
EXAMPLE ELEMENTAL UN
EXAMPLE PERFORMANCE
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IN-FLIGHT THRUST MEA
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ILLUSTRATION OF MATH
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ILLUSTRATION OF MATH
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FLIGHT TEST MEASUREM
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TWO-TAILED 95% STUDE
TWO-TAILED STUDENT'S
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DECISION LOGIC DIAGR
MEASUREMENTS USED IN
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INFLUENCE COEFFICIEN
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EXAMPLE PERFORMANCE
EFFECT OF THE NUMBER
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FICTITIOUS EXAMPLE D

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