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GYC: A program to compute the turbulent boundary layer on a rotating coneA computer program, GYC, which is capable of computing the properties of a compressible turbulent boundary layer on a rotating axisymmetric cone-cylinder body, according to the principles of invariant modeling was studied. The program is extended to include the calculation of the turbulence scale by a differential equation. GYC is in operation on the CDC-7600 computer and has undergone several corrections and improvements as a result of the experience gained. The theoretical basis for the program and the method of implementation, as well as information on its operation are given.
Document ID
19770013077
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sullivan, R. D.
(Aeronautical Research Associates of Princeton, Inc. Princeton, NJ, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-151981
WORKING PAPER-76-2
Report Number: NASA-CR-151981
Report Number: WORKING PAPER-76-2
Accession Number
77N20021
Funding Number(s)
CONTRACT_GRANT: NAS2-8014
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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