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Fundamental Aeronautics Program: Overview of Project Work in Supersonic Cruise EfficiencyThe Supersonics Project, part of NASA?s Fundamental Aeronautics Program, contains a number of technical challenge areas which include sonic boom community response, airport noise, high altitude emissions, cruise efficiency, light weight durable engines/airframes, and integrated multi-discipline system design. This presentation provides an overview of the current (2011) activities in the supersonic cruise efficiency technical challenge, and is focused specifically on propulsion technologies. The intent is to develop and validate high-performance supersonic inlet and nozzle technologies. Additional work is planned for design and analysis tools for highly-integrated low-noise, low-boom applications. If successful, the payoffs include improved technologies and tools for optimized propulsion systems, propulsion technologies for a minimized sonic boom signature, and a balanced approach to meeting efficiency and community noise goals. In this propulsion area, the work is divided into advanced supersonic inlet concepts, advanced supersonic nozzle concepts, low fidelity computational tool development, high fidelity computational tools, and improved sensors and measurement capability. The current work in each area is summarized.
Document ID
20110011565
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Castner, Raymond
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
March 15, 2011
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-17750
Report Number: E-17750
Meeting Information
Meeting: 2011 Technical Conference
Location: Cleveland, OH
Country: United States
Start Date: March 15, 2011
End Date: March 17, 2011
Funding Number(s)
WBS: WBS 984754.02.07.03.13.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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