MARC record from Internet Archive

LEADER: 02335cam 2200433 a 4500
001 ocm78052247
003 OCoLC
005 20100714083906.0
008 820624s1981 caua bt f000 0 eng d
035 $a
035 $a
037 $aADA106061
040 $aCMontNP$cAD#$dAD#
049 $aAD#A
086 0 $aD 208.14/2:NPS-67-81-010
088 $aNPS-67-81-010
100 1 $aBinn, Brian A.
245 10 $aCombustion behavior of solid fuel ramjets, vol. 1. Correlation of reacting and non-reacting flow characteristics /$cBrian A. Binn, Winston E. Scott, David W. Netzer.
260 $aMonterey, Calif. :$bNaval Postgraduate School,$c1981.
300 $aviii, 58 p. :$bill. ;$c28 cm.
500 $a"NPS-67-81-010."
500 $aCover title.
500 $a"July 1981."
500 $a"Prepared for: Naval Weapons Center; China Lake, CA 93555."
504 $aIncludes bibliographic references (p. 57)
506 $a"Approved for public release; distribution is unlimited."
513 $aTechnical report; 1981.
520 $aAn experimental investigation was conducted to determine the relationship between the cold flow characteristics of velocity, pressure distribution, and turbulence intensity and the reacting flow performance and combustion characteristics of a solid fuel ramjet. The effects of configuration and air flow changes on the above characteristics were examined. Average regression rates and combustion efficiencies were not significantly affected by changes in configuration. These variations in test conditions significantly affected the centerline turbulence intensity but not the near-wall turbulence intensity in cold flow. Near-wall turbulence profiles in cold flow were found to correlate with the fuel regression profiles in reacting flows. The use of bypass resulted in decreases in regression rate and efficiencies for all cases. (Author)
650 0 $aSolid propellants$xCombustion.
650 0 $aAirplanes$xRamjet engines$xCombustion.
650 0 $aFluid dynamics.
700 1 $aScott, Winston E.
700 1 $aNetzer, David Willis,$d1939-
710 2 $aNaval Postgraduate School (U.S.)
994 $aC0$bAD#
035 $a
035 $a
949 $lgen$nL$aTL709.3.R3$bB64$s1$tnorm$u00001$i32768000465751
926 $aNPS-LIB$bDIGIPROJ$cD 208.14/2:NPS-67-81-010$dTECH_RPT$eNEVER$f1