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Computation of supersonic viscous flows over ogive-cylinders at angle of attackThe parabolic Navier-Stokes (PNS) marching finite-difference method is applied to 3-D viscous flow over pointed ogive-cylinders, and to turbulent flow over a cone. Ogive computations were performed using the new technique recently reported by Vigneron, Rakich, and Tannehill. Comparison is made with experiment and inviscid computations. The present results show that this method, which neglects part of the pressure gradient in the x-momentum equation, is nevertheless valid for flows with a strong favorable pressure gradient. In addition, turbulent separated flow over a cone has been computed using the older PNS code due to Lubard and Helliwell. It is found that one must freeze the turbulent eddy-viscosity model upstream of 3-D separation to get agreement with experiment.
Document ID
19790039504
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rakich, J. V.
(NASA Ames Research Center Moffett Field, CA, United States)
Vigneron, Y. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Agarwal, R.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 79-0131
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: New Orleans, LA
Start Date: January 15, 1979
End Date: January 17, 1979
Sponsors: American Institute of Aeronautics, Astronautics
Accession Number
79A23517
Funding Number(s)
CONTRACT_GRANT: NGR-16-002-038
Distribution Limits
Public
Copyright
Other

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