Static Performance Of Six Innovative Thrust Reverser Concepts For Subsonic Transport Applications Summary Of The Nasa Langley Innovative Thrust Reverser Test Program
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Static Performance Of Six Innovative Thrust Reverser Concepts For Subsonic Transport Applications Summary Of The Nasa Langley Innovative Thrust Reverser Test Program
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Author :
language : en
Publisher: DIANE Publishing
Release Date : 2000
Static Performance Of Six Innovative Thrust Reverser Concepts For Subsonic Transport Applications Summary Of The Nasa Langley Innovative Thrust Reverser Test Program written by and has been published by DIANE Publishing this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000 with categories.
Static Performance Of Six Innovative Thrust Reverser Concepts For Subsonic Transport Applications
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Author : Scott C. Asbury
language : en
Publisher:
Release Date : 2000
Static Performance Of Six Innovative Thrust Reverser Concepts For Subsonic Transport Applications written by Scott C. Asbury and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000 with Aerodynamics categories.
The NASA Langley Configuration Aerodynamics Branch has conducted an experimental investigation to study the static performance of innovative thrust reverser concepts applicable to high-bypass-ratio turbofan engines. Testing was conducted on a conventional separate-flow exhaust system configuration, a conventional cascade thrust reverser configuration, and six innovative thrust reverser configurations. The innovative thrust reverser configurations consisted of a cascade thrust reverser with porous fan-duct blocker, a blockerless thrust reverser, two core-mounted target thrust reversers, a multi-door crocodile thrust reverser, and a wing-mounted thrust reverser. Each of the innovative thrust reverser concepts offer potential weight savings and/or design simplifications over a conventional cascade thrust reverser design. Testing was conducted in the Jet-Exit Test facility at NASA Langley Research Center using a 7.9% scale exhaust system model with a fan-to-core bypass ratio of approximately 9.0. All tests were conducted with no external flow and cold, high-pressure air was used to simulate core and fan exhaust flows. Results show that the innovative thrust reverser concepts achieved thrust reverser performance levels which, when taking into account the potential for system simplification and reduced weight, may make them competitive with, or potentially more cost effective than current state-of-the-art thrust reverser systems.
Static Performance Of Six Innovative Thrust Reverser Concepts For Subsonic Transport Applications
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-06-27
Static Performance Of Six Innovative Thrust Reverser Concepts For Subsonic Transport Applications 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 2018-06-27 with categories.
The NASA Langley Configuration Aerodynamics Branch has conducted an experimental investigation to study the static performance of innovative thrust reverser concepts applicable to high-bypass-ratio turbofan engines. Testing was conducted on a conventional separate-flow exhaust system configuration, a conventional cascade thrust reverser configuration, and six innovative thrust reverser configurations. The innovative thrust reverser configurations consisted of a cascade thrust reverser with porous fan-duct blocker, a blockerless thrust reverser, two core-mounted target thrust reversers, a multi-door crocodile thrust reverser, and a wing-mounted thrust reverser. Each of the innovative thrust reverser concepts offer potential weight savings and/or design simplifications over a conventional cascade thrust reverser design. Testing was conducted in the Jet-Exit Test Facility at NASA Langley Research Center using a 7.9%-scale exhaust system model with a fan-to-core bypass ratio of approximately 9.0. All tests were conducted with no external flow and cold, high-pressure air was used to simulate core and fan exhaust flows. Results show that the innovative thrust reverser concepts achieved thrust reverser performance levels which, when taking into account the potential for system simplification and reduced weight, may make them competitive with, or potentially more cost effective than current state-of-the-art thrust reverser systems. Asbury, Scott C. and Yetter, Jeffrey A. Langley Research Center RTOP 522-25-31-01...
Future Propulsion Systems And Energy Sources In Sustainable Aviation
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Author : Saeed Farokhi
language : en
Publisher: John Wiley & Sons
Release Date : 2020-01-21
Future Propulsion Systems And Energy Sources In Sustainable Aviation written by Saeed Farokhi and has been published by John Wiley & Sons this book supported file pdf, txt, epub, kindle and other format this book has been release on 2020-01-21 with Technology & Engineering categories.
A comprehensive review of the science and engineering behind future propulsion systems and energy sources in sustainable aviation Future Propulsion Systems and Energy Sources in Sustainable Aviation is a comprehensive reference that offers a review of the science and engineering principles that underpin the concepts of propulsion systems and energy sources in sustainable air transportation. The author, a noted expert in the field, examines the impact of air transportation on the environment and reviews alternative jet fuels, hybrid-electric and nuclear propulsion and power. He also explores modern propulsion for transonic and supersonic-hypersonic aircraft and the impact of propulsion on aircraft design. Climate change is the main driver for the new technology development in sustainable air transportation. The book contains critical review of gas turbine propulsion and aircraft aerodynamics; followed by an insightful presentation of the aviation impact on environment. Future fuels and energy sources are introduced in a separate chapter. Promising technologies in propulsion and energy sources are identified leading to pathways to sustainable aviation. To facilitate the utility of the subject, the book is accompanied by a website that contains illustrations, and equation files. This important book: Contains a comprehensive reference to the science and engineering behind propulsion and power in sustainable air transportation Examines the impact of air transportation on the environment Covers alternative jet fuels and hybrid-electric propulsion and power Discusses modern propulsion for transonic, supersonic and hypersonic aircraft Examines the impact of propulsion system integration on aircraft design Written for engineers, graduate and senior undergraduate students in mechanical and aerospace engineering, Future Propulsion Systems and Energy Sources in Sustainable Aviation explores the future of aviation with a guide to sustainable air transportation that includes alternative jet fuels, hybrid-electric propulsion, all-electric and nuclear propulsion.
Static Performance Of Six Innovative Thrust Reverser Concets For Subsonic Transport Applications
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Author : Scott C. Asbury
language : en
Publisher:
Release Date : 2000
Static Performance Of Six Innovative Thrust Reverser Concets For Subsonic Transport Applications written by Scott C. Asbury and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000 with categories.
Nasa Langley Scientific And Technical Information Output 2000
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Author :
language : en
Publisher:
Release Date : 2001
Nasa Langley Scientific And Technical Information Output 2000 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2001 with categories.
Innovation In Flight
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Author : Joseph R. Chambers
language : en
Publisher:
Release Date : 2005
Innovation In Flight written by Joseph R. Chambers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2005 with Aeronautics categories.
Nasa Sp
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Author :
language : en
Publisher:
Release Date : 1992
Nasa Sp 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 Aeronautics categories.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1994
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Aeronautics categories.
Aeronautical Engineering A Cumulative Index To A Continuing Bibliography
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Author :
language : en
Publisher:
Release Date : 1988
Aeronautical Engineering A Cumulative Index To A Continuing Bibliography written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1988 with categories.