Analysis and testing of high entrainment single nozzle jet pumps with variable mixing tubes

LDR 02934cam a2200457Ia 4500
001 011431361
003 MiAaHDL
005 20141013010000.0
006 m d
007 cr bn ---auaua
008 060626s1972 dcua bt f000 0 eng d
024 8 ⊔ ‡a19720020347
024 8 ⊔ ‡aN7227997
024 8 ⊔ ‡a72N27997
035 ⊔ ⊔ ‡asdr-uiuc6385964
035 ⊔ ⊔ ‡a(OCoLC)70185074
040 ⊔ ⊔ ‡aFER ‡cFER ‡dOCLCG
049 ⊔ ⊔ ‡aUIUU
100 1 ⊔ ‡aHickman, Kenneth E.
245 1 0 ‡aAnalysis and testing of high entrainment single nozzle jet pumps with variable mixing tubes / ‡cKenneth E. Hickman, Philip G. Hill, and Gerald B. Gilbert.
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service [distributor], ‡c1972.
300 ⊔ ⊔ ‡aiii, 137 p. : ‡bill. ; ‡c27 cm.
490 ⊔ 0 ‡aNASA contractor report ; ‡vNASA CR-2067
500 ⊔ ⊔ ‡a"NASA CR-2067."
500 ⊔ ⊔ ‡a"June 1972."
500 ⊔ ⊔ ‡aCover title.
504 ⊔ ⊔ ‡aIncludes bibliographical references (p. 116).
520 ⊔ ⊔ ‡aAn analytical model was developed to predict the performance characteristics of axisymmetric single-nozzle jet pumps with variable area mixing tubes. The primary flow may be subsonic or supersonic. The computer program uses integral techniques to calculate the velocity profiles and the wall static pressures that result from the mixing of the supersonic primary jet and the subsonic secondary flow. An experimental program was conducted to measure mixing tube wall static pressure variations, velocity profiles, and temperature profiles in a variable area mixing tube with a supersonic primary jet. Static pressure variations were measured at four different secondary flow rates. These test results were used to evaluate the analytical model. The analytical results compared well to the experimental data. Therefore, the analysis is believed to be ready for use to relate jet pump performance characteristics to mixing tube design.
530 ⊔ ⊔ ‡aAlso available via Internet from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 6/21/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19720020347%5f1972020347.pdf.
536 ⊔ ⊔ ‡aPrepared by Dynatech R/D Company, Cambridge, Mass. for Langley Research Center ‡bNAS 2-5845
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 7 ‡aTest equipment. ‡2nasat
650 ⊔ 7 ‡aPressure measurement. ‡2nasat
650 ⊔ 7 ‡aNumerical analysis. ‡2nasat
650 ⊔ 7 ‡aComputer programs. ‡2nasat
650 ⊔ 7 ‡aPerformance prediction. ‡2nasat
650 ⊔ 7 ‡aNozzle geometry. ‡2nasat
650 ⊔ 7 ‡aNozzle flow. ‡2nasat
650 ⊔ 7 ‡aJet pumps. ‡2nasat
700 1 ⊔ ‡aGilbert, Gerald B.
700 1 ⊔ ‡aHill, Philip G. ‡q(Philip Graham), ‡d1932-
710 2 ⊔ ‡aLangley Research Center.
710 2 ⊔ ‡aDynatech R/D Company.
CID ⊔ ⊔ ‡a011431361
DAT 0 ⊔ ‡a20101027105026.0 ‡b20141013010000.0
DAT 1 ⊔ ‡a20141112173021.0 ‡b2024-01-20T19:13:20Z
CAT ⊔ ⊔ ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
FMT ⊔ ⊔ ‡aBK
HOL ⊔ ⊔ ‡0sdr-uiuc6385964 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106629063 ‡sUIU ‡16385964
974 ⊔ ⊔ ‡bUIU ‡cUIUC ‡d20240120 ‡sgoogle ‡uuiug.30112106629063 ‡y1972 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2019