Analysis of laminar boundary layers on right circular cones at angle of attack, including streamline-swallowing effects

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035 ⊔ ⊔ ‡a(MiU)99187625424106381
035 ⊔ ⊔ ‡asdr-miu.99187625424106381
035 ⊔ ⊔ ‡a(OCoLC)18059426
035 ⊔ ⊔ ‡a(GWLA)gwla ocm18059426
040 ⊔ ⊔ ‡aVPI ‡beng ‡erda ‡cVPI ‡dOCLCQ ‡dOCLCF ‡dOCLCO ‡dOCLCQ ‡dCOD ‡dOCLCO ‡dOCLCQ ‡dTRAAL
049 ⊔ ⊔ ‡aMAIN
050 ⊔ 4 ‡aTL574.B6 ‡bM34 1972
086 0 ⊔ ‡aD 301.45/33:72-134
100 1 ⊔ ‡aMayne, Arloe Wesley, ‡cJr., ‡eauthor.
245 1 0 ‡aAnalysis of laminar boundary layers on right circular cones at angle of attack, including streamline-swallowing effects / ‡cArloe Wesley Mayne, Jr.
264 ⊔ 1 ‡aArnold Air Force Station, Tennessee : ‡bVon Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, ‡c1972.
300 ⊔ ⊔ ‡ax, 95 pages : ‡billustrations ; ‡c27 cm
336 ⊔ ⊔ ‡atext ‡btxt ‡2rdacontent
337 ⊔ ⊔ ‡aunmediated ‡bn ‡2rdamedia
338 ⊔ ⊔ ‡avolume ‡bnc ‡2rdacarrier
490 0 ⊔ ‡aAEDC-TR ; ‡v72-134
500 ⊔ ⊔ ‡a"Final report - September 1970 to April 1972."
500 ⊔ ⊔ ‡a"ARO-VKF-TR-72-117."
500 ⊔ ⊔ ‡a"October 1972."
504 ⊔ ⊔ ‡aIncludes bibliographical references (pages 93-95).
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 ‡aBoundary layer.
710 2 ⊔ ‡aARO, Inc.
710 2 ⊔ ‡aArnold Engineering Development Center.
899 ⊔ ⊔ ‡a39015104952679
CID ⊔ ⊔ ‡a102892932
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