SAE AIR 1678 : 2016
SAE AIR 1678 : 2016
UNCERTAINTY OF IN-FLIGHT THRUST DETERMINATION
SAE International
Table of Contents
1. SCOPE
2. REFERENCES
3. GLOSSARY
4. MEASUREMENT UNCERTAINTY METHODOLOGY
5. IN-FLIGHT THRUST MEASUREMENT PROCESSES
6. APPLICATION OF UNCERTAINTY METHODOLOGY TO THE
IN-FLIGHT THRUST PROGRAM
APPENDIX A - SMALL SAMPLE STATISTICAL METHODS
APPENDIX B - IMPACT OF MEASUREMENT PROCESS ON ERROR
CLASSIFICATION AND ESTIMATION
APPENDIX C - EXAMPLE INFLUENCE COEFFICIENT CALCULATIONS
APPENDIX D - INITIAL PERFORMANCE SURVEY OF THRUST
MEASUREMENT OPTIONS
APPENDIX E - CALIBRATED MATHEMATICAL MODEL AND THE ASSOCIATED
UNCERTAINTY COMPONENTS FOR FLIGHT TESTS
APPENDIX F - NONSYMMETRIC UNCERTAINTIES
APPENDIX G - BACKGROUND OF UNCERTAINTY METHODOLOGY
Abstract
Describes and illustrates the process for determination of uncertainty of turbofan and turbojet engine in-flight thrust and other measured in-flight performance parameters.
General Product Information
| Document Type | Standard |
| Status | Current |
| Publisher | SAE International |
| Committee | E-33 |
