• SAE AIR 5450 : 2014

    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

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

    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

    Abstract - (Show below) - (Hide below)

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

    General Product Information - (Show below) - (Hide below)

    Committee E-33
    Document Type Standard
    Publisher SAE International
    Status Current
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    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

    Standards Referencing This Book - (Show below) - (Hide below)

    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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