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Numerical Analysis of Intra-Cavity and Power-Stream Flow Interaction in Multiple Gas-Turbine Disk-CavitiesA numerical analysis methodology and solutions of the interaction between the power stream and multiply-connected multi-cavity sealed secondary flow fields are presented. Flow solutions for a multi-cavity experimental rig were computed and compared with experimental data of Daniels and Johnson. The flow solutions illustrate the complex coupling between the main-path and the cavity flows as well as outline the flow thread that exists throughout the subplatform multiple cavities and seals. The analysis also shows that the de-coupled solutions on single cavities is inadequate. The present results show trends similar to the T-700 engine data that suggests the changes in the CDP seal altered the flow fields throughout the engine and affected the engine performance.
Document ID
19950021923
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Athavale, M. M.
(CFD Research Corp. Huntsville, AL., United States)
Przekwas, A. J.
(CFD Research Corp. Huntsville, AL., United States)
Hendricks, R. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Steinetz, B. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1995
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:106886
E-9523
NASA-TM-106886
Meeting Information
Meeting: Turbo Expo 1995
Location: Houston, TX
Country: United States
Start Date: June 5, 1995
End Date: June 8, 1995
Accession Number
95N28344
Funding Number(s)
PROJECT: RTOP 242-50-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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