MARC record from Internet Archive

LEADER: 02409cam 2200541 a 4500
001 ocm35591971
003 OCoLC
005 20100714112134.5
006 m b
007 cr cga---uuuuu
008 960919s1968 caua b f000 0 eng d
035 $a
035 $a
037 $aAD0673249$bDTI
040 $aVPI$cVPI$dOCLCG$dAD#
049 $aAD#A
086 0 $aD 208.14/2:NPS-59SL8061A
088 $aNPS-59SL8061A
100 1 $aSarpkaya, Turgut,$d1928-
245 14 $aThe deflection of plane turbulent jets by convex walls /$cby Turgut Sarpkaya.
260 $aMonterey, California :$bNaval Postgraduate School,$c1968.
300 $a54 p. :$bill. ;$c28 cm.
500 $aTitle from cover.
500 $a"27 June 1968"--Cover.
500 $a"NPS-59SL8061A"--Cover.
500 $aDTIC Identifiers: Bistable amplifiers, graphs (charts)
500 $aAuthor(s) key words: Coanda effect, turbulent jet atatchment, jet attachment to curved walls, deflection of plane turbulent jets by convex walls.
504 $aIncludes bibliographical references (p. 23-24)
506 $a"Approved for public release; distribution unlimited"--Cover.
513 $aTechnical report; 1968.
520 $aThe effects of geometry and Reynolds number on the attachment of a jet to a convex wall and the mechanism of high pressure recovery in convex-walled amplifiers are investigated. The results are presented in terms of normalized parameters in a form suitable for comparison with theoretical results. Reasonably good agreement is obtained between the experimental results and those predicted theoretically by Gortler and Glauert, particularly for regions of flow away from the control port. The effects of the wall setback and control port are most pronounced in a region near the power nozzle where u sub m/u sub o attains values as high as 1.25.
650 0 $aFluid dynamics.
650 0 $aFluid amplifiers.
650 0 $aJets$xFluid dynamics.
710 2 $aNaval Postgraduate School (U.S.)
994 $aC0$bAD#
035 $a
035 $a
035 $a
035 $a
035 $a
035 $a
035 $a
592 $ack/ 10/6/09.
035 $a
949 $lgen$nL$aQA911$b.S2$s1$tnorm$u00001$i32768001699580
926 $aNPS-LIB$bDIGIPROJ$cD 208.14/2:NPS-59SL8061A$dTECH_RPT$eNEVER$f1
926 $aNPS-LIB$bDIGIPROJ$cD 208.14/2:NPS-59SL8061A$dTECH_RPT$eNEVER$f2