NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Intake Noise Generation: Source MechanismsNo abstract available
Document ID
20150010399
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Envia, Ed
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
June 10, 2015
Publication Date
November 14, 2011
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-664221
Report Number: E-664221
Meeting Information
Meeting: Engine Intake Aerothermal Design: Subsonic to High Speed Application
Location: Rhode-St-Genýse
Country: Belgium
Start Date: November 14, 2011
End Date: November 16, 2011
Sponsors: Von Karman Inst. for Fluid Dynamics
Funding Number(s)
WBS: WBS 561581.02.08.03.45.02.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available