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Analysis of single- and two-phase flows in turbopump inducers.Single-phase and two-phase cavitating flow regime performance of liquid propellant rocket engine turbopump inducers
Document ID
19670036624
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cooper, P.
Date Acquired
August 3, 2013
Publication Date
November 1, 1966
Subject Category
Auxiliary Systems
Report/Patent Number
ASME PAPER 66-WA/FE-23
Report Number: ASME PAPER 66-WA/FE-23
Accession Number
67A15353
Funding Number(s)
CONTRACT_GRANT: NAS8-4006
CONTRACT_GRANT: NAS3-2573
Distribution Limits
Public
Copyright
Other
Keywords
SINGLE-PHASE FLOW
CAVITATION FLOW
TURBOPUMP
INDUCER
TWO-PHASE FLOW
LIQUID PROPELLANT ROCKET ENGINE

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