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Development of an Efficient CFD Model for Nuclear Thermal Thrust Chamber Assembly DesignThe objective of this effort is to develop an efficient and accurate computational methodology to predict both detailed thermo-fluid environments and global characteristics of the internal ballistics for a hypothetical solid-core nuclear thermal thrust chamber assembly (NTTCA). Several numerical and multi-physics thermo-fluid models, such as real fluid, chemically reacting, turbulence, conjugate heat transfer, porosity, and power generation, were incorporated into an unstructured-grid, pressure-based computational fluid dynamics solver as the underlying computational methodology. The numerical simulations of detailed thermo-fluid environment of a single flow element provide a mechanism to estimate the thermal stress and possible occurrence of the mid-section corrosion of the solid core. In addition, the numerical results of the detailed simulation were employed to fine tune the porosity model mimic the pressure drop and thermal load of the coolant flow through a single flow element. The use of the tuned porosity model enables an efficient simulation of the entire NTTCA system, and evaluating its performance during the design cycle.
Document ID
20070031967
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Cheng, Gary
(Alabama Univ. Birmingham, AL, United States)
Ito, Yasushi
(Alabama Univ. Birmingham, AL, United States)
Ross, Doug
(Alabama Univ. Birmingham, AL, United States)
Chen, Yen-Sen
(Engineering Sciences, Inc. Huntsville, AL, United States)
Wang, Ten-See
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 23, 2013
Publication Date
June 25, 2007
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: 39th AIAA Thermophysics Conference
Location: Miami, FL
Country: United States
Start Date: June 27, 2007
End Date: June 28, 2007
Sponsors: American Inst. of Aeronautics and Astronautics, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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