Analysis of the three-dimensional compressible turbulent boundary layer on a sharp cone at incidence in supersonic and hypersonic flow

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035 ⊔ ⊔ ‡a(MiU)99187625471906381
035 ⊔ ⊔ ‡asdr-miu.99187625471906381
035 ⊔ ⊔ ‡a(OCoLC)18059349
035 ⊔ ⊔ ‡a(GWLA)gwla ocm18059349
040 ⊔ ⊔ ‡aVPI ‡beng ‡erda ‡cVPI ‡dOCLCQ ‡dOCLCF ‡dOCLCO ‡dOCLCQ ‡dOCLCO ‡dOCLCQ ‡dTRAAL
049 ⊔ ⊔ ‡aMAIN
050 ⊔ 4 ‡aTL574.B6 ‡bA3 1972
086 0 ⊔ ‡aD 301.45/33:72-066
100 1 ⊔ ‡aAdams, John C., ‡eJr., ‡eauthor.
245 1 0 ‡aAnalysis of the three-dimensional compressible turbulent boundary layer on a sharp cone at incidence in supersonic and hypersonic flow / ‡cJohn C. Adams, Jr.
264 ⊔ 1 ‡aArnold Air Force Base, Tennessee : ‡bVon Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, ‡c1972.
300 ⊔ ⊔ ‡ax, 82 pages : ‡billustrations ; ‡c27 cm
336 ⊔ ⊔ ‡atext ‡btxt ‡2rdacontent
337 ⊔ ⊔ ‡aunmediated ‡bn ‡2rdamedia
338 ⊔ ⊔ ‡avolume ‡bnc ‡2rdacarrier
490 0 ⊔ ‡aAEDC-TR ; ‡v72-066
500 ⊔ ⊔ ‡aReport was prepared by ARO, Inc., a subsidiary of Sverdrup & Parcel and Associates, Inc.
500 ⊔ ⊔ ‡a"Final Report : July 1971 to February 1972."
500 ⊔ ⊔ ‡a"June 1972"--Cover
504 ⊔ ⊔ ‡aIncludes bibliographical references (pages 33-38).
520 ⊔ ⊔ ‡aAn analytical approach toward numerical calculation of the three-dimensional turbulent boundary layer on a sharp cone at incidence under supersonic and hypersonic flow conditions is presented. The theoretical model is based on implicit finite-difference integration of the governing three-dimensional turbulent boundary-layer equations in conjunction with a three-dimensional scalar eddy-viscosity model of turbulence. Comparison is made of present theory with detailed experimental measurements of the three-dimensional turbulent boundary-layer structure (velocity and temperature profiles), the surface streamline direction (obtained via an oil-flow technique) and surface heat-transfer rate.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 7 ‡aBoundary layer. ‡2fast ‡0(OCoLC)fst00837095
650 ⊔ 7 ‡aAerodynamics, Supersonic. ‡2fast ‡0(OCoLC)fst00798221
650 ⊔ 7 ‡aAerodynamics, Hypersonic. ‡2fast ‡0(OCoLC)fst00798215
650 ⊔ 6 ‡aAérodynamique hypersonique. ‡0(CaQQLa)201-0080662
650 ⊔ 6 ‡aAérodynamique supersonique. ‡0(CaQQLa)201-0000388
650 ⊔ 6 ‡aCouche limite. ‡0(CaQQLa)201-0009010
650 ⊔ 0 ‡aAerodynamics, Hypersonic.
650 ⊔ 0 ‡aAerodynamics, Supersonic.
650 ⊔ 0 ‡aTurbulent boundary layer.
650 ⊔ 0 ‡aSpace vehicles ‡xAtmospheric entry.
710 2 ⊔ ‡aARO, Inc., ‡esponsor.
710 2 ⊔ ‡aArnold Engineering Development Center, ‡esponsor.
710 1 ⊔ ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body.
730 0 ⊔ ‡aTechnical Report Archive & Image Library (TRAIL)
899 ⊔ ⊔ ‡a39015104952323
CID ⊔ ⊔ ‡a102893092
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DAT 1 ⊔ ‡a20230928062550.0 ‡b2024-07-29T17:35:40Z
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