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Dish stirling solar receiver combustor test program

Authors :
Bankston, C. P
Back, L. H
Publication Year :
1981
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1981.

Abstract

The operational and energy transfer characteristics of the Dish Stirling Solar Receiver (DSSR) combustor/heat exchanger system was evaluated. The DSSR is designed to operate with fossil fuel augmentation utilizing a swirl combustor and cross flow heat exchanger consisting of a single row of 4 closely spaced tubes that are curved into a conical shape. The performance of the combustor/heat exchanger system without a Stirling engine was studied over a range of operating conditions and output levels using water as the working fluid. Results show that the combustor may be started under cold conditions, controlled safety, and operated at a constant air/fuel ratio (10 percent excess air) over the required range of firing rates. Furthermore, nondimensional heat transfer coefficients based on total heat transfer are plotted versus Reynolds number and compared with literature data taken for single rows of closely spaced tubes perpendicular to cross flow. The data show enhanced heat transfer for the present geometry and test conditions. Analysis of the results shows that the present system meets specified thermal requirements, thus verifying the feasibility of the DSSR combustor design for final prototype fabrication.

Subjects

Subjects :
Energy Production And Conversion

Details

Language :
English
Database :
NASA Technical Reports
Notes :
DE-AI01-81ET-20307, , JPL PROJ. 5105-76, , NAS7-100
Publication Type :
Report
Accession number :
edsnas.19820005622
Document Type :
Report