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Computation of hypersonic flows with finite rate condensation and evaporation of waterA computer program for modelling 2D hypersonic flows of gases containing water vapor and liquid water droplets is presented. The effects of interphase mass, momentum and energy transfer are studied. Computations are compared with existing quasi-1D calculations on the nozzle of the NASA Langley Eight Foot High Temperature Tunnel, a hypersonic wind tunnel driven by combustion of natural gas in oxygen enriched air.
Document ID
19930040878
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Perrell, Eric R.
(North Carolina State Univ. Raleigh, United States)
Candler, Graham V.
(Minnesota Univ. Minneapolis, United States)
Erickson, Wayne D.
(NASA Langley Research Center Hampton, VA, United States)
Wieting, Alan R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 93-0796
Meeting Information
Meeting: AIAA, Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 11, 1993
End Date: January 14, 1993
Sponsors: AIAA
Accession Number
93A24875
Funding Number(s)
CONTRACT_GRANT: NAG1-1330
CONTRACT_GRANT: NAGW-1331
Distribution Limits
Public
Copyright
Other

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