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220628s1975 tnua bt f000 0 eng d |
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‡a(MiU)99187625990806381
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‡asdr-miu.99187625990806381
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‡a(OCoLC)1333449628
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‡aTRAAL
‡beng
‡erda
‡cTRAAL
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‡aMAIN
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‡aD 301.45/33: 75-097
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‡aStarr, R. F.,
‡eauthor.
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‡aExperiments to assess the influence of changes in the tunnel wall boundary layer on transonic wall crossflow characteristics /
‡cR.F. Starr.
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‡aArnold Air Force Base, Tennessee :
‡bArnold Engineering Development Center, Air Force Systems Command, United States Air Force,
‡c1975.
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‡a30 pages :
‡billustrations ;
‡c28 cm
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‡atext
‡btxt
‡2rdacontent
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‡aunmediated
‡bn
‡2rdamedia
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‡avolume
‡bnc
‡2rdacarrier
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‡aAEDC-TR ;
‡v75-097
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‡aReport was prepared by ARO, Inc., a subsidiary of Sverdrup & Parcel and Associates, Inc.
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‡a"Final Report for Period November 1974 -- January 1975."
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‡a"November 1975."
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‡aIncludes bibliographical references (pages 29-29).
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‡aThe equivalent porosity of the test section wall in a transonic wind tunnel with a fixed geometric porosity and varying wall boundary-layer displacement thickness, has been investigated. Previous experiments have demonstrated that the boundary-layer displacement thickness on the wall influences the wall crossflow characteristic. Experimental data from a Ludwieg tube type of transonic tunnel are compared with data from conventional transonic tunnels in the Mach number range from 0.95 to 1.15. The displacement thickness studied is comparatively thin and represents typical values which will be encountered in future high Reynolds number transonic tunnels.
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‡aMode of access: Internet.
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‡aTransonic wind tunnels.
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‡aWind tunnel walls.
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‡aWall pressure (Aerodynamics)
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‡aARO, Inc.,
‡esponsor.
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‡aArnold Engineering Development Center,
‡esponsor.
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‡aUnited States.
‡bAir Force.
‡bSystems Command,
‡eissuing body.
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‡aTechnical Report Archive & Image Library (TRAIL)
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