SAE AIR 5450 : 2014
Current
The latest, up-to-date edition.
ADVANCED DUCTED PROPULSOR IN-FLIGHT THRUST DETERMINATION
Hardcopy , PDF
English
09-06-2014
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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