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SAE AIR 5450 : 2014

Current

Current

The latest, up-to-date edition.

ADVANCED DUCTED PROPULSOR IN-FLIGHT THRUST DETERMINATION

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

09-06-2014

€191.67
Excluding VAT

1. SCOPE
2. REFERENCES AND NOMENCLATURE
3. DEFINITIONS AND METHODOLOGY
4. ENGINE CONCEPTUAL DESIGN AND CONFIGURATIONS
5. INSTALLATION CONSIDERATIONS
6. THRUST METHOD OPTIONS
7. AERODYNAMIC AND PROPULSION TESTING
8. IN-FLIGHT THRUST VALIDATION
9. THRUST UNCERTAINTY ANALYSIS
10. OTHER OPERATING MODES REQUIRING CONSIDERATION
APPENDIX A - ADP IN FLIGHT THRUST CALCULATION, BPR = 6
APPENDIX B - ADP IN FLIGHT THRUST CALCULATION, BPR = 12
APPENDIX C - ADP IN FLIGHT THRUST CALCULATION, BPR = 15
APPENDIX D - GENERALIZED THRUST - LOW ROTOR SPEED
             (N[1,R]) COORELATION USING ATF BYPASS RATIO 6
             ENGINE AT CRUISE CONDITIONS
APPENDIX E - GENERALIZED THRUST - LOW ROTOR SPEED
             (N[1,R]) COORELATION USING ATF BYPASS RATIO 12
             ENGINE AT CRUISE CONDITIONS
APPENDIX F - GENERALIZED THRUST - LOW ROTOR SPEED
             (N[1,R]) COORELATION USING ATF BYPASS RATIO 15
             ENGINE AT CRUISE CONDITIONS
APPENDIX G - GENERALIZED THRUST - LOW ROTOR SPEED
             (N[1,R]) COORELATION USING ATF BYPASS RATIO 6
             ENGINE AT TAKEOFF CONDITIONS
APPENDIX H - GENERALIZED THRUST - LOW ROTOR SPEED
             (N[1,R]) COORELATION USING ATF BYPASS RATIO 12
             ENGINE AT TAKEOFF CONDITIONS
APPENDIX I - GENERALIZED THRUST - LOW ROTOR SPEED
             (N[1,R]) COORELATION USING ATF BYPASS RATIO 15
             ENGINE AT TAKEOFF CONDITIONS
APPENDIX J - GENERALIZED THRUST - FUEL FLOW (W[F,R])
             COORELATION USING ATF BYPASS RATIO 6 ENGINE
             AT CRUISE CONDITIONS
APPENDIX K - GENERALIZED THRUST - FUEL FLOW (W[F,R])
             COORELATION USING ATF BYPASS RATIO 12 ENGINE
             AT CRUISE CONDITIONS
APPENDIX L - GENERALIZED THRUST - FUEL FLOW (W[F,R])
             COORELATION USING ATF BYPASS RATIO 15 ENGINE
             AT CRUISE CONDITIONS
APPENDIX M - GENERALIZED THRUST - FUEL FLOW (W[F,R])
             COORELATION USING ATF BYPASS RATIO 6 ENGINE
             AT TAKEOFF CONDITIONS
APPENDIX N - GENERALIZED THRUST - FUEL FLOW (W[F,R])
             COORELATION USING ATF BYPASS RATIO 12 ENGINE
             AT TAKEOFF CONDITIONS
APPENDIX O - GENERALIZED THRUST - FUEL FLOW (W[F,R])
             COORELATION USING ATF BYPASS RATIO 15 ENGINE
             AT TAKEOFF CONDITIONS
APPENDIX P - GENERALIZED THRUST - CORE ENGINE
             PRESSURE RATIO (CEPR) COORELATION USING ATF
             BYPASS RATIO 6 ENGINE AT CRUISE CONDITIONS
APPENDIX Q - GENERALIZED THRUST - CORE ENGINE
             PRESSURE RATIO (CEPR) COORELATION USING ATF
             BYPASS RATIO 12 ENGINE AT CRUISE CONDITIONS
APPENDIX R - GENERALIZED THRUST - CORE ENGINE
             PRESSURE RATIO (CEPR) COORELATION USING ATF
             BYPASS RATIO 15 ENGINE AT CRUISE CONDITIONS
APPENDIX S - GENERALIZED THRUST - CORE ENGINE
             PRESSURE RATIO (CEPR) COORELATION USING ATF
             BYPASS RATIO 6 ENGINE AT TAKEOFF CONDITIONS
APPENDIX T - GENERALIZED THRUST - CORE ENGINE
             PRESSURE RATIO (CEPR) COORELATION USING ATF
             BYPASS RATIO 12 ENGINE AT TAKEOFF CONDITIONS
APPENDIX U - GENERALIZED THRUST - CORE ENGINE
             PRESSURE RATIO (CEPR) COORELATION USING ATF
             BYPASS RATIO 15 ENGINE AT TAKEOFF CONDITIONS
APPENDIX V - GENERALIZED THRUST - TORQUE (TRQ[L])
             COORELATION USING ATF BYPASS RATIO 6 ENGINE AT
             CRUISE CONDITIONS
APPENDIX W - GENERALIZED THRUST - TORQUE (TRQ[L])
             COORELATION USING ATF BYPASS RATIO 12 ENGINE AT
             CRUISE CONDITIONS
APPENDIX X - GENERALIZED THRUST - TORQUE (TRQ[L])
             COORELATION USING ATF BYPASS RATIO 15 ENGINE AT
             CRUISE CONDITIONS
APPENDIX Y - GENERALIZED THRUST - TORQUE (TRQ[L])
             COORELATION USING ATF BYPASS RATIO 6 ENGINE AT
             TAKEOFF CONDITIONS
APPENDIX Z - GENERALIZED THRUST - TORQUE (TRQ[L])
             COORELATION USING ATF BYPASS RATIO 12 ENGINE AT
             TAKEOFF CONDITIONS
APPENDIX AA - GENERALIZED THRUST - TORQUE (TRQ[L])
              COORELATION USING ATF BYPASS RATIO 15 ENGINE AT
              TAKEOFF CONDITIONS
APPENDIX BB - GAS PATH/NOZZLE METHOD USING ATF BYPASS
              RATIO 6 ENGINE AT CRUISE CONDITIONS
APPENDIX CC - GAS PATH/NOZZLE METHOD USING ATF BYPASS
              RATIO 12 ENGINE AT CRUISE CONDITIONS
APPENDIX DD - GAS PATH/NOZZLE METHOD USING ATF BYPASS
              RATIO 15 ENGINE AT CRUISE CONDITIONS
APPENDIX EE - GAS PATH/NOZZLE METHOD USING ATF BYPASS
              RATIO 6 ENGINE AT TAKEOFF CONDITIONS
APPENDIX FF - GAS PATH/NOZZLE METHOD USING ATF BYPASS
              RATIO 12 ENGINE AT TAKEOFF CONDITIONS
APPENDIX GG - GAS PATH/NOZZLE METHOD USING ATF BYPASS
              RATIO 15 ENGINE AT TAKEOFF CONDITIONS
APPENDIX HH - GAS PATH/NOZZLE METHOD USING GLTF AND
              RESIDUAL ERROR (RERR) BYPASS RATIO 6 ENGINE AT
              CRUISE CONDITIONS
APPENDIX II - GAS PATH/NOZZLE METHOD USING GLTF AND
              RESIDUAL ERROR (RERR) BYPASS RATIO 12 ENGINE AT
              CRUISE CONDITIONS
APPENDIX JJ - GAS PATH/NOZZLE METHOD USING GLTF AND
              RESIDUAL ERROR (RERR) BYPASS RATIO 15 ENGINE AT
              CRUISE CONDITIONS
APPENDIX KK - GAS PATH/NOZZLE METHOD USING GLTF AND
              RESIDUAL ERROR (RERR) BYPASS RATIO 6 ENGINE AT
              TAKEOFF CONDITIONS
APPENDIX LL - GAS PATH/NOZZLE METHOD USING GLTF AND
              RESIDUAL ERROR (RERR) BYPASS RATIO 12 ENGINE AT
              TAKEOFF CONDITIONS
APPENDIX MM - GAS PATH/NOZZLE METHOD USING GLTF AND
              RESIDUAL ERROR (RERR) BYPASS RATIO 15 ENGINE AT
              TAKEOFF CONDITIONS

Describes methods and the additional challenges to the thrust determination for these ADP engines.

Committee
E-33
DocumentType
Standard
Pages
392
PublisherName
SAE International
Status
Current
Supersedes

SAE AIR 6007 : 2016 IN-FLIGHT THRUST DETERMINATION FOR AIRCRAFT WITH THRUST VECTORING
SAE AIR 5771 : 2018 THE MEASUREMENT OF ENGINE THRUST IN AN ALTITUDE TEST FACILITY
SAE AIR 1703 : 2012 IN-FLIGHT THRUST DETERMINATION
SAE AIR 1678 : 2016 UNCERTAINTY OF IN-FLIGHT THRUST DETERMINATION
SAE AIR 6064 : 2018 REVERSE THRUST

SAE AIR 1703 : 2012 IN-FLIGHT THRUST DETERMINATION
SAE AIR 1678 : 2016 UNCERTAINTY OF IN-FLIGHT THRUST DETERMINATION
SAE AS 755 : 2014 AIRCRAFT PROPULSION SYSTEM PERFORMANCE STATION DESIGNATION
SAE AIR 4065 : 2012 PROPELLER/PROPFAN IN-FLIGHT THRUST DETERMINATION
SAE AIR 5020 : 2012 TIME-DEPENDENT IN-FLIGHT THRUST DETERMINATION
SAE ARP 4990B : 2015 TURBINE FLOWMETER FUEL FLOW CALCULATIONS

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