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Performance of a modular combustor designed for a VTOL tip-turbine lift fanCombustion efficiency and performance of swirl can modules under conditions simulating operation of 10,000 pound thrust lift engine for vertical takeoff
Document ID
19710029291
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Marchionna, N. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1971
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-6542
E-6441
Report Number: NASA-TN-D-6542
Report Number: E-6441
Accession Number
71N38767
Funding Number(s)
PROJECT: RTOP 721-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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