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200908s1982 ohua b f000 0 eng d |
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‡a(MiU)99187539741206381
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‡aD 301.45/57:82-3075
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‡aPurohit, S. C.,
‡eauthor.
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‡aNumerical simulation of flow around a three-dimensional turret /
‡cS.C. Purohit, J.S.
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‡aWright-Patterson Air Force Base, Ohio :
‡bFlight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force,
‡c1982.
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‡a53 pages :
‡billustrations ;
‡c28 cm
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‡atext
‡btxt
‡2rdacontent
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‡aunmediated
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‡aAFWAL-TR (Air Force Wright Aeronautical Laboratories) ;
‡v82-3075
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‡a"Final report for period May 1981- April 1982."
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‡a"November 1982."
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‡aIncludes bibliographic references (pages 52-53).
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‡aThe compressible Navier-Stokes equations in mass averaged variables are numerically solved for flow around a surface mounted turret. The three-dimensional unsteady separated flow is investigated with emphasis on the near wake region. The computation is performed on the CRAY-1 computer using MacCormack's explicit finite difference scheme. For the free stream Mach number 0.55 and Reynolds number 10.3 x 1,000,000/m, the time dependent calculation is carried out for 55,800 grid points in the computational domain to achieve steady state periodic solution. The entire flow field around the turret is analyzed and the comparison with available experimental data is reported. (Author).
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‡aWork performed by University of Dayton Research Institute, Dayton, Ohio, for the United States Air Force under contract
‡bF33615-79-C-3030.
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‡aMode of access: Internet.
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‡aWakes (Aerodynamics)
‡xMathematical models..
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‡aNavier-Stokes equations.
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‡aAir Force Flight Dynamics Laboratory (U.S.),
‡esponsor.
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‡aAir Force Wright Aeronautical Laboratories,
‡esponsor.
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‡aTechnical Report Archive & Image Library (TRAIL)
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