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Analysis of effect of tail-pipe-burner design parameters on thrust-augmentation
Document ID
19740075148
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Manganiello, E. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 7, 2013
Publication Date
October 28, 1948
Publication Information
Publication: NACA Conf. on Turbojet-Eng. Thrust-Augmentation Res.
Subject Category
General
Accession Number
74N73087
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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