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CAVE3: A general transient heat transfer computer code utilizing eigenvectors and eigenvaluesThe method of solution is a hybrid analytical numerical technique which utilizes eigenvalues and eigenvectors. The method is inherently stable, permitting large time steps even with the best of conductors with the finest of mesh sizes which can provide a factor of five reduction in machine time compared to conventional explicit finite difference methods when structures with small time constants are analyzed over long time periods. This code will find utility in analyzing hypersonic missile and aircraft structures which fall naturally into this class. The code is a completely general one in that problems involving any geometry, boundary conditions and materials can be analyzed. This is made possible by requiring the user to establish the thermal network conductances between nodes. Dynamic storage allocation is used to minimize core storage requirements. This report is primarily a user's manual for CAVE3 code. Input and output formats are presented and explained. Sample problems are included which illustrate the usage of the code as well as establish the validity and accuracy of the method.
Document ID
19780010416
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Palmieri, J. V.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Rathjen, K. A.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1978
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-145290
Report Number: NASA-CR-145290
Accession Number
78N18359
Funding Number(s)
CONTRACT_GRANT: NAS1-14643
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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