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AST Combustion Workshop: Diagnostics Working Group ReportA workshop was convened under NASA's Advanced Subsonics Technologies (AST) Program. Many of the principal combustion diagnosticians from industry, academia, and government laboratories were assembled in the Diagnostics/Testing Subsection of this workshop to discuss the requirements and obstacles to the successful implementation of advanced diagnostic techniques to the test environment of the proposed AST combustor. The participants, who represented the major relevant areas of advanced diagnostic methods currently applied to combustion and related fields, first established the anticipated AST combustor flowfield conditions. Critical flow parameters were then examined and prioritized as to their importance to combustor/fuel injector design and manufacture, environmental concerns, and computational interests. Diagnostic techniques were then evaluated in terms of current status, merits and obstacles for each flow parameter. All evaluations are presented in tabular form and recommendations are made on the best-suited diagnostic method to implement for each flow parameter in order of applicability and intrinsic value.
Document ID
19970001580
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Locke, Randy J. (NYMA, Inc. Brook Park, OH United States)
Hicks, Yolanda R. (NASA Lewis Research Center Cleveland, OH United States)
Hanson, Ronald K. (Stanford Univ. CA United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1996
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-107354
NAS 1.15:107354
E-10508
Accession Number
97N11374
Funding Number(s)
PROJECT: RTOP 538-06-12
CONTRACT_GRANT: NAS3-27186
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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