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Non-Contacting Compliant Foil Seal for Gas Turbine EngineThe program is aimed at enhancing the existing analysis to include the turbulence effect. Several manufacturing methods are being investigated in order to apply our know-how in building the seal hardware. The contents include: 1) Test Facilities; 2) Analysis Enhancements; 3) Accomplishments/Status; and 4) Materials Study.
Document ID
20020091975
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Salehi, Mohsen (Mohawk Innovative Technology, Inc. Albany, NY United States)
Heshmat, Hooshang (Mohawk Innovative Technology, Inc. Albany, NY United States)
Date Acquired
August 20, 2013
Publication Date
October 1, 2002
Publication Information
Publication: 2001 NASA Seal/Secondary Air System Workshop
Volume: 1
Subject Category
Mechanical Engineering
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle20020091964Collected Works2001 NASA Seal/secondary Air System Workshop, Volume 1
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