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JANNAF liquid rocket combustion instability panel research recommendationsThe Joint Army, Navy, NASA, Air Force (JANNAF) Liquid Rocket Combustion Instability Panel was formed in 1988, drawing its members from industry, academia, and government experts. The panel was charted to address the needs of near-term engine development programs and to make recommendations whose implementation would provide not only sufficient data but also the analysis capabilities to design stable and efficient engines. The panel was also chartered to make long-term recommendations toward developing mechanistic analysis models that would not be limited by design geometry or operating regime. These models would accurately predict stability and thereby minimize the amount of subscale testing for anchoring. The panel has held workshops on acoustic absorbing devices, combustion instability mechanisms, instability test hardware, and combustion instability computational methods. At these workshops, research projects that would meet the panel's charter were suggested. The JANNAF Liquid Rocket Combustion Instability Panel's conclusions about the work that needs to be done and recommendations on how to approach it, based on evaluation of the suggested research projects, are presented.
Document ID
19910004178
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Klem, Mark D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-5826
NASA-TM-103653
NAS 1.15:103653
Report Number: E-5826
Report Number: NASA-TM-103653
Report Number: NAS 1.15:103653
Meeting Information
Meeting: JANNAF Combustion Meeting
Location: Cheyenne, WY
Country: United States
Start Date: November 5, 1990
End Date: November 9, 1990
Accession Number
91N13491
Funding Number(s)
PROJECT: RTOP 506-42-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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