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Supersonic viscous flow over cones at incidenceThe conically symmetric Navier-Stokes equations are solved by MacCormack's method for the supersonic flow past sharp cones at incidence. To provide closure for the case of turbulent flows, a scalar eddy-viscosity model based on mixing length hypotheses is used. The results are compared with available experimental data.
Document ID
19810036796
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Mcrae, D. S. (USAF, Flight Dynamics Laboratory, Moffett Field Calif., United States)
Hussaini, M. Y. (NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1979
Subject Category
Aerodynamics
Meeting Information
Meeting: International Conference on Numerical Methods in Fluid Dynamics
Location: Tiflis
Country: Georgian
Start Date: June 21, 1978
End Date: June 24, 1978
Accession Number
81A21200
Distribution Limits
Public
Copyright
Other

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