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Numerical studies of the fluid and optical fields associated with complex cavity flowsNumerical solutions for the flowfield about several cavity configurations have been computed using the Reynolds averaged Navier-Stokes equations. Comparisons between numerical and experimental results are made in two dimensions for free shear layers and a rectangular cavity, and in three dimensions for the transonic aero-window problem of the Stratospheric Observatory for Infrared Astronomy (SOFIA). Results show that dominant acoustic frequencies and magnitudes of the self excited resonant cavity flows compare well with the experiment. In addition, solution sensitivity to artificial dissipation and grid resolution levels are determined. Optical path distortion due to the flow field is modelled geometrically and is found to match the experiment. The fluid field was computed using a diagonalized scheme within an overset mesh framework. An existing code, OVERFLOW, was utilized with the additions of characteristic boundary condition and output routines required for reduction of the unsteady data. The newly developed code is directly applicable to a generalized three dimensional structured grid zone. Details are provided in a paper included in Appendix A.
Document ID
19920014963
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Atwood, Christopher A.
(MCAT Inst. San Jose, CA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1992
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-190295
NAS 1.26:190295
REPT-92-007
Report Number: NASA-CR-190295
Report Number: NAS 1.26:190295
Report Number: REPT-92-007
Accession Number
92N24206
Funding Number(s)
CONTRACT_GRANT: NCC2-677
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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