AIAA G-045-2003 Assessing Experimental Uncertainty Supplement to AIAA S-071A-1999《对AIAA S-071A-1999评估实验的不确定性补充》.pdf
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1、GuideAssessing Experimental Uncertainty Supplement to AIAA S-071A-1999AIAA standards are copyrighted by the American Institute of Aeronautics andAstronautics (AIAA), 1801 Alexander Bell Drive, Reston, VA 20191-4344 USA. All rightsreserved.AIAA grants you a license as follows: The right to download a
2、n electronic file of this AIAAstandard for temporary storage on one computer for purposes of viewing, and/or printingone copy of the AIAA standard for individual use. Neither the electronic file nor the hardcopy print may be reproduced in any way. In addition, the electronic file may not bedistribut
3、ed elsewhere over computer networks or otherwise. The hard copy print may onlybe distributed to other employees for their internal use within your organization.AIAAG-045-2003AIAAG-045-2003GuideAssessing Experimental Uncertainty Supplement to AIAA S-071A-1999Sponsored byAmerican Institute of Aeronaut
4、ics and AstronauticsAbstractThis AIAA Guide supplements the methodology for assessment of experimental uncertainties andtechniques for evaluating experimental error sources provided in AIAA Standard S-071A-1999,“Assessment of Experimental Uncertainty with Application to Wind Tunnel Testing.“ This do
5、cumentprovides additional information and examples to assist the experimentalist in performing an uncertaintyanalysis. Its focus is on helping the experimenter begin to apply uncertainty analysis techniques. Theinformation contained in the standard and this guide is not limited to wind tunnel testin
6、git can be appliedto a wide range of experiments.AIAA G-045-2003iiLibrary of Congress Cataloging-in-Publication DataGuide : assessing experimental uncertainty : supplement to AIAAS-071A-1999 / sponsored by American Institute of Aeronautics andAstronautics.p. cm.Includes bibliographical references.IS
7、BN 1-56347-663-0 (hardcopy) - ISBN 1-56347-664-9 (electronic)1. Wind tunnels. 2. Airplanes-Models-Testing-Standards. 3.Uncertainty (Information theory) I. Title: Assessing experimentaluncertainty. II. American Institute of Aeronautics and Astronautics.III. Assessment of experimental uncertainty with
8、 application to windtunnel testing.TL567.W5A87 1999 Suppl.629.13452-dc222003024006Published byAmerican Institute of Aeronautics and Astronautics1801 Alexander Bell Drive, Suite 500, Reston, VA 20191-4344Copyright 2003 American Institute of Aeronautics andAstronauticsAll rights reserved.No part of th
9、is publication may be reproduced in any form, in an electronic retrievalsystem or otherwise, without prior written permission of the publisher.Printed in the United State of AmericaAIAA G-045-2003iiiCONTENTSForeword.vDedication viPart I Basic Topics. 11 Introduction 12 Uncertainty Methodology and Ap
10、plication 22.1 Methodology Primer . 22.1.1 Single Test 42.1.2 Multiple Tests 42.1.3 Relative Sensitivity Factors 52.2 Application Primer. 52.2.1 Experiment Definition . 52.2.2 Uncertainties of the Experimental Results. 62.2.2.1 Multiple Tests 62.2.2.2 Single Test 93 General Uncertainty Analysis Exam
11、pleEvaluating Measurement Methods. 113.1 Introduction . 113.2 Mach Number Equations 113.3 Uncertainty Analysis. 123.3.1 Partial Derivative Terms . 133.3.2 Transducer Uncertainty 143.3.3 Mach Number Uncertainty 143.3.4 Relative Sensitivity Factors 164 General Uncertainty Analysis ExampleEvaluating Da
12、ta Reduction Equations . 184.1 Turbine Efficiency Equations 194.2 Procedure . 194.3 Results 204.3.1 Overall Uncertainty . 204.3.2 UMF. 204.3.3 UPC. 214.3.4 Summary. 225 Systematic Uncertainties and Correlation. 305.1 Systematic Uncertainties 305.2 Correlated Systematic Uncertainties 325.2.1 Bath Uni
13、formity . 335.2.2 Standard Uncertainty 34AIAA G-045-2003iv5.3 Correlated Systematic Uncertainties Example 34Part II Advanced Topics 386 Random Uncertainties and Correlation. 386.1 Random Uncertainties 386.2 Correlated Random Uncertainty Example . 386.2.1 Background. 386.2.2 Calibration Approach and
14、Results . 396.2.3 Uncertainty Analysis. 406.3 Discharge Coefficient and Mass Flow Rate Equations . 447 Regression Uncertainty . 477.1 Categories of Regression Uncertainty . 477.1.1 Uncertainty in Coefficients 487.1.2 Uncertainty in Y from Regression Model . 487.1.3 (Xi, Yi) Variables are Functions 4
15、97.2 Linear Regression Uncertainty. 497.2.1 General Approach. 497.2.2 Reporting Regression Uncertainties 517.2.3 Differential Pressure Transducer Calibration Example . 527.2.4 X and Y as Functional Relations 547.2.5 1stOrder Regressions. 567.2.5.1 Uncertainty in Coefficients 567.2.5.2 Classical Regr
16、ession Random Uncertainty . 587.2.5.3 Lift Slope and Lift Coefficient Example 598 Automated Uncertainty Analysis for Production Experiments . 648.1 Introduction . 648.2 Error Propagation . 648.3 Estimation of Input Uncertainties . 658.3.1 Systematic Uncertainty Estimation 668.3.2 Random Uncertainty
17、Estimation. 678.3.3 Specific Uncertainty Estimates. 678.4 Results 688.5 Summary. 689 Useful References . 79AIAA G-045-2003vForewordExperimental uncertainty is a complex subject involving both statistical techniques and engineeringjudgment. In 1995 the AIAA Standards Technical Council approved an AIA
18、A Standard on experimentaluncertainty that was revised in 1999 (AIAA S-071A-1999, “Assessment of Experimental Uncertainty withApplication to Wind Tunnel Testing“). The AIAA adopted the contents of an Advisory Report (AR-304) setforth by the Advisory Group for Aerospace Research and Development (AGAR
19、D). The AIAA Standarddefines a rational and practical framework for quantifying and reporting experimental uncertainty andpresents the application of the methodology to wind tunnel testing. This AIAA Guide supplements thestandard. It provides additional information and examples to assist the experim
20、entalist in performing anuncertainty analysis. Its focus is on helping the experimenter begin to apply uncertainty analysistechniques.The AIAA Standards Procedures provide that all approved Standards, Recommended Practices, andGuides are advisory only. Their use by anyone engaged in industry or trad
21、e is entirely voluntary. Thereis no agreement to adhere to any AIAA standards publication and no commitment to conform to or beguided by a standards report. In formulating, revising, and approving standards publications, theCommittees on Standards will not consider patents that may apply to the subj
22、ect matter. Prospectiveusers of the publications are responsible for protecting themselves against liability for infringement ofpatents or copyrights, or both.The Standards Subcommittee of the AIAA Ground Test Technical Committee (Mr. E.A. Arrington,Chairperson) had many members who contributed to t
23、his document over the course of its preparation.The following individuals should be recognized for their contributions:Gregory Addington, Chairperson Air Force Research LabDavid M. Cahill Sverdrup Tech., AEDCJulie Carlile Air Force Research LabDaniel Cresci GASLSusan T. Hudson, Technical Editor-in-C
24、hiefMississippi State UniversityWayne Kalliomaa Air Force Research LabJerry Kegelman NASA Langley Research CenterDaniel E. Marren AEDC/White OakLaura J. McGill RaytheonThomas McLaughlin U.S. Air Force AcademyJulie Morrow U.S. Air Force AcademyMathew L. Rueger BoeingWilliam A. Straka Applied Research
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