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Supersonics N+2 System Validation Nozzle Test: GE Inverted Velocity Profile Nozzle ConceptNo abstract available
Document ID
20150010383
Document Type
Presentation
Authors
Martens, Steve (GE Global Research Center Irvine, CA, United States)
Morgenstern, John (Lockheed Martin Corp. Bethesda, MD, United States)
Bridges, James (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
June 10, 2015
Publication Date
October 18, 2011
Subject Category
Acoustics
Aircraft Design, Testing And Performance
Aircraft Propulsion And Power
Report/Patent Number
E-663280
Meeting Information
Meeting: NASA Acoustics Technical Working Group Meeting
Location: Hampton, VA
Country: United States
Start Date: October 18, 2011
End Date: October 19, 2011
Funding Number(s)
WBS: WBS 984754.02.07.03.17.08.01
Distribution Limits
Public
Copyright
Public Use Permitted.

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