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Evaluation Of Various Thrust Calibration I E Calculation Techniques On An F404 Engine


Evaluation Of Various Thrust Calibration I E Calculation Techniques On An F404 Engine
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Evaluation Of Various Thrust Calibration I E Calculation Techniques On An F404 Engine


Evaluation Of Various Thrust Calibration I E Calculation Techniques On An F404 Engine
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Author : Ronald J. Ray
language : en
Publisher:
Release Date : 1990

Evaluation Of Various Thrust Calibration I E Calculation Techniques On An F404 Engine written by Ronald J. Ray and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1990 with Airplanes categories.




Evaluation Of Various Thrust Calculation Techniques On An F404 Engine


Evaluation Of Various Thrust Calculation Techniques On An F404 Engine
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Author : Ronald J. Ray
language : en
Publisher:
Release Date : 1990

Evaluation Of Various Thrust Calculation Techniques On An F404 Engine written by Ronald J. Ray and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1990 with categories.




Flight Evaluation Of A Simplified Gross Thrust Calculation Technique Using An F100 Turbofan Engine In An F 15 Airplane


Flight Evaluation Of A Simplified Gross Thrust Calculation Technique Using An F100 Turbofan Engine In An F 15 Airplane
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Author : Frank J. Kurtenbach
language : en
Publisher:
Release Date : 1981

Flight Evaluation Of A Simplified Gross Thrust Calculation Technique Using An F100 Turbofan Engine In An F 15 Airplane written by Frank J. Kurtenbach and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1981 with categories.




Airflow Calibration And Exhaust Pressure Temperature Survey Of An F404 S N 215 109 Turbofan Engine


Airflow Calibration And Exhaust Pressure Temperature Survey Of An F404 S N 215 109 Turbofan Engine
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-25

Airflow Calibration And Exhaust Pressure Temperature Survey Of An F404 S N 215 109 Turbofan Engine written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-25 with categories.


A General Electric F-404 turbofan engine was calibrated for thrust and airflow at the NASA Lewis Propulsion System Laboratory in support of future flight tests of the X-29 aircraft. Tests were conducted with and without augmentation, over a range of flight conditions, including the two design points of the airplane. Data obtained during the altitude tests will be used to correct two independent gross thrust calculation routines which will be installed and operated on the airplane to determine in-flight gross thrust. Corrected airflow data as a function of corrected fan speed collapsed onto a single curve. Similarly, trends were observed and defined for both augmented and dry thrust. Overall agreement between measured data and F-404 Engine Spec Deck data was within 2 percent for airflow and 6 percent for thrust. The results of an uncertainty analysis for thrust and airflow is presented. In addition to the thrust calibration, the exhaust gas boundary layer pressure and temperatures were surveyed at selected condition and engine power levels to obtain data for another NASA F-404 program. Test data for these surveys are presented. Burns, Maureen E. and Kirchgessner, Thomas A. Glenn Research Center NASA-TM-100159, E-3447, NAS 1.15:100159 RTOP 505-62-3B



Evaluation Of A Simplified Gross Thrust Calculation Technique Using Two Prototype F100 Turbofan Engines In An Altitude Facility


Evaluation Of A Simplified Gross Thrust Calculation Technique Using Two Prototype F100 Turbofan Engines In An Altitude Facility
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Author : Frank J. Kurtenbach
language : en
Publisher:
Release Date : 1979

Evaluation Of A Simplified Gross Thrust Calculation Technique Using Two Prototype F100 Turbofan Engines In An Altitude Facility written by Frank J. Kurtenbach and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with Airplanes categories.




Validation Of The Gas Generator Method Of Calculating Jet Engine Thrust And Evaluation Of Xb 70 1 Airplane Engine Performance At Ground Static Conditons


Validation Of The Gas Generator Method Of Calculating Jet Engine Thrust And Evaluation Of Xb 70 1 Airplane Engine Performance At Ground Static Conditons
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Author : Henry H. Arnaiz
language : en
Publisher:
Release Date : 1970

Validation Of The Gas Generator Method Of Calculating Jet Engine Thrust And Evaluation Of Xb 70 1 Airplane Engine Performance At Ground Static Conditons written by Henry H. Arnaiz and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Aerodynamic measurements categories.


Deficiencies in established techniques of measuring aircraft thrust in flight led to the application of the gas generator method of calculating engine thrust to the XB-70-1 airplane. A series of tests on a ground static-thrust stand [were]performed on the airplane to establish at ground static conditions the accuracy of this method, to measure the installed thrust of the YJ93-GE-3 engine, and to determine the effect of instrumentation errors and nonuniform flows at the engine compressor face on the thrust calculation. Tests with an aerodynamically choked inlet, an opened inlet-bypass system, and varying combinations of operating engines were also conducted. Results showed that the accuracy of the gas generator method was ±2 percent for the normal operation of the XB-70-1 airplane at ground static conditions and for the upper 70 percent of the engine's throttle range. They also showed that the effect of individual instrument errors on the thrust calculation was reduced because of the large number of measurements and that abnormally high inlet flow distortion affects the thrust calculation. When corrected for inlet losses, the installed thrust of the YJ93-GE-3 engine agreed favorably with the engine manufacturer's uninstalled estimated thrust for all power settings except those at the low end.--P. [i].



Measurement Effects On The Calculation Of In Flight Thrust For An F404 Turbofan Engine


Measurement Effects On The Calculation Of In Flight Thrust For An F404 Turbofan Engine
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Author : Timothy E. Conners
language : en
Publisher:
Release Date : 1989

Measurement Effects On The Calculation Of In Flight Thrust For An F404 Turbofan Engine written by Timothy E. Conners and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Airplanes categories.




Asme Technical Papers


Asme Technical Papers
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Author :
language : en
Publisher:
Release Date :

Asme Technical Papers written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Mechanical engineering categories.




Paper


Paper
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Author :
language : en
Publisher:
Release Date : 1992

Paper written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Mechanical engineering categories.




Government Reports Announcements Index


Government Reports Announcements Index
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Author :
language : en
Publisher:
Release Date : 1992-12

Government Reports Announcements Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992-12 with Science categories.