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An improved model for two-dimensional turbulent base flow with zero mass bleed Summary reportModel for two-dimensional turbulent base flow with zero mass bleed applicable to multinozzle rocket
Document ID
19660012150
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lamb, J. P. (Texas Univ. Austin, TX, United States)
Lenzo, C. S. (Texas Univ. Austin, TX, United States)
Date Acquired
August 3, 2013
Publication Date
February 28, 1966
Subject Category
Space Sciences
Report/Patent Number
NASA-CR-71527
Report Number: NASA-CR-71527
Accession Number
66N21439
Funding Number(s)
CONTRACT_GRANT: NAS8-11482
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET NOZZLE
TURBULENT FLOW
BASE FLOW
TWO-DIMENSIONAL FLOW
MATHEMATICAL MODEL

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