| Record ID | marc_columbia/Columbia-extract-20221130-007.mrc:448563722:1809 |
| Source | marc_columbia |
| Download Link | /show-records/marc_columbia/Columbia-extract-20221130-007.mrc:448563722:1809?format=raw |
LEADER: 01809fam a22003498a 4500
001 3438918
005 20221020073917.0
008 021010s2003 nyu 001 0 eng
010 $a 2002038572
020 $a0791801926
035 $a(OCoLC)50803655
035 $a(OCoLC)ocm50803655
035 $9AVS6995CU
035 $a(NNC)3438918
035 $a3438918
040 $aDLC$cDLC$dDLC$dNNC$dOrLoB-B
042 $apcc
050 00 $aTJ267.5.C5$bA94 2003
082 00 $a621.5/1$221
100 1 $aAungier, Ronald H.$0http://id.loc.gov/authorities/names/n99052384
245 10 $aAxial-flow compressors :$ba strategy for aerodynamic design and analysis /$cRonald H. Aungier.
260 $aNew York :$bASME Press,$c2003.
263 $a0301
300 $axiii, 361 pages :$billustrations ;c ;$c24 cm
336 $atext$btxt$2rdacontent
337 $aunmediated$bn$2rdamedia
500 $aIncludes index.
504 $aIncludes bibliographical references (p. [349]-354) and index.
505 00 $g1.$tIntroduction -- $g2.$tThermodynamics -- $g3.$tFluid Mechanics -- $g4.$tAxial-Flow Compressor Blade Profiles -- $g5.$tTwo-Dimensional Blade-to-Blade Flow Through Cascades of Blades -- $g6.$tEmpirical Performance Models Based on Two-Dimensional Cascade Tests -- $g7.$tMeridional Through-Flow Analysis -- $g8.$tEnd-Wall Boundary Layer Analysis -- $g9.$tAerodynamic Performance Analysis -- $g10.$tCompressor Stage Aerodynamic Design -- $g11.$tMultistage Axial-Flow Compressor Aerodynamic Design -- $g12.$tQuasi-Three-Dimensional Blade Passage Flow Field Analysis -- $g13.$tOther Components and Variations.
650 0 $aAxial flow compressors$xAerodynamics.$0http://id.loc.gov/authorities/subjects/sh2008008195
650 0 $aAxial flow compressors$xDesign and construction.
852 00 $boff,eng$hTJ267.5.C5$iA94 2003