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The future challenge for aeropropulsionNASA's research in aeropropulsion is focused on improving the efficiency, capability, and environmental compatibility for all classes of future aircraft. The development of innovative concepts, and theoretical, experimental, and computational tools provide the knowledge base for continued propulsion system advances. Key enabling technologies include advances in internal fluid mechanics, structures, light-weight high-strength composite materials, and advanced sensors and controls. Recent emphasis has been on the development of advanced computational tools in internal fluid mechanics, structural mechanics, reacting flows, and computational chemistry. For subsonic transport applications, very high bypass ratio turbofans with increased engine pressure ratio are being investigated to increase fuel efficiency and reduce airport noise levels. In a joint supersonic cruise propulsion program with industry, the critical environmental concerns of emissions and community noise are being addressed. NASA is also providing key technologies for the National Aerospaceplane, and is studying propulsion systems that provide the capability for aircraft to accelerate to and cruise in the Mach 4-6 speed range. The combination of fundamental, component, and focused technology development underway at NASA will make possible dramatic advances in aeropropulsion efficiency and environmental compatibility for future aeronautical vehicles.
Document ID
19920015921
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rosen, Robert
(NASA Headquarters Washington, DC United States)
Bowditch, David N.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-6943
NAS 1.15:105613
NASA-TM-105613
Report Number: E-6943
Report Number: NAS 1.15:105613
Report Number: NASA-TM-105613
Meeting Information
Meeting: Aeroengine 1992
Location: Moscow
Country: USSR
Start Date: April 6, 1992
End Date: April 12, 1992
Accession Number
92N25164
Funding Number(s)
PROJECT: RTOP 505-62-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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