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Rolls-Royce Low Noise Highly Variable Cycle Nozzle for Next Generation Supersonic AircraftAn overview of the work performed by Rolls-Royce under contract NNL08AA29C is presented. The work includes computational fluid dynamic (CFD) analysis for, and design of, a highly variable cycle exhaust model for the Supersonic project (NRA NN06ZEA001N). The CFD analysis shows that the latest design improvements to the clam shell doors have increased flow through the ejector over that achieved with previous designs.
Document ID
20080047730
Document Type
Conference Paper
Authors
Sokhey, Jack S. (LibertyWorks United States)
Kube-McDowell, Matthew (Purdue Univ. United States)
Date Acquired
August 24, 2013
Publication Date
October 7, 2008
Subject Category
Fluid Mechanics and Thermodynamics
Report/Patent Number
E-16793
Meeting Information
Fundamental Aeronautics Annual Meeting(Atlanta, GA)
Funding Number(s)
WBS: WBS 984754.02.07.03.17.04
CONTRACT_GRANT: NNL08AA29C
Distribution Limits
Public
Copyright
Public Use Permitted.

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