High Stability Engine Control Histec Flight Test Results Nasa Tm 1998 208481 Oct 26 1998
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Author | : United States. National Aeronautics and Space Administration |
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Download High Stability Engine Control (HISTEC) Flight Test Results... NASA/TM-1998-208481... Oct. 26, 1998 Book in PDF, Epub and Kindle
Author | : United States. National Aeronautics and Space Administration |
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Release | : 1999* |
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Download HIGH STABILITY ENGINE CONTROL (HISTEC): FLIGHT DEMONSTRATION RESULTS... NASA/TM-1998-208655... JAN. 20, 1999 Book in PDF, Epub and Kindle
Author | : United States. National Aeronautics and Space Administration |
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Download THE HIGH STABILITY ENGINE CONTROL (HISTEC) PROGRAM: FLIGHT DEMONSTRATION PHASE... NASA/TM-1998-208482... SEP. 15, 1998 Book in PDF, Epub and Kindle
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Total Pages | : 16 |
Release | : 1998 |
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Download High Stability Engine Control (HISTEC) Flight Test Results Book in PDF, Epub and Kindle
Author | : United States. National Aeronautics and Space Administration |
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Download DEVELOPMENT AND TESTING OF A HIGH STABILITY ENGINE CONTROL (HISTEC) SYSTEM... NASA/TM-1998-206562... OCT. 27, 1998 Book in PDF, Epub and Kindle
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Total Pages | : 18 |
Release | : 1998 |
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Download The High Stability Engine Control (HISTEC) Program: Flight Demonstration Phase Book in PDF, Epub and Kindle
Author | : John S. Orme |
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Total Pages | : 20 |
Release | : 1998 |
Genre | : Airplanes |
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Download Development and Testing of a High Stability Engine Control (HISTEC) System Book in PDF, Epub and Kindle
Author | : Robert D. Southwick |
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Release | : 1998 |
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Download The High Stability Engine Control (HISTEC) Program Flight Test Results Book in PDF, Epub and Kindle
Author | : John C. DeLaat |
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Total Pages | : 11 |
Release | : 1998 |
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Download High Stability Engine Control (HISTEC): Flight Demonstration Results Book in PDF, Epub and Kindle
Future aircraft turbine engines, both commercial and military, must be able to accommodate expected increased levels of steady-state and dynamic engine-face distortion. The current approach of incorporating sufficient design stall margin to tolerate these increased levels of distortion would significantly reduce performance. The High Stability Engine Control (HISTEC) program has developed technologies for an advanced, integrated engine control system that uses measurement-based estimates of distortion to enhance engine stability. The resulting distortion tolerant control reduces the required design stall margin, with a corresponding increase in performance and/or decrease in fuel burn. The HISTEC concept was successfully flight demonstrated on the F-15 ACTIVE aircraft during the summer of 1997. The flight demonstration was planned and carried out in two parts, the first to show distortion estimation, and the second to show distortion accommodation. Post-flight analysis shows that the HISTEC technologies are able to successfully estimate and accommodate distortion, transiently setting the stall margin requirement on-line and in real-time. Flight demonstration of the HISTEC technologies has significantly reduced the risk of transitioning the technology to tactical and commercial engines.
Author | : United States. National Aeronautics and Space Administration |
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Release | : 1999* |
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Download FLIGHT STABILITY AND CONTROL AND PERFORMANCE RESULTS FROM THE LINEAR AEROSPIKE SR-71 EXPERIMENT (LASRE)... NASA/TM-1998-206565... OCT. 26, 1998 Book in PDF, Epub and Kindle