<![CDATA[PKK Library Search for 'au:"Runckel,Jack F"']]>

<![CDATA[PKK Library Search for 'au:"Runckel,Jack F"']]> /cgi-bin/koha/opac-search.pl?q=ccl=au%3A%22Runckel%2CJack%20F%22&format=rss2 6 0 200 HYDROGEN PEROXIDE HOT-JET SIMULATOR FOR WIND-TUNNEL TESTS OF TURBOJET-EXIT MODELS ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=393199 By Runckel,Jack F. Nasa, Washington, D.C. 1959 . 35 , Bound With Nasa Memo 1-2-59l-1-10-59l

Place Hold on HYDROGEN PEROXIDE HOT-JET SIMULATOR FOR WIND-TUNNEL TESTS OF TURBOJET-EXIT MODELS

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=393199 EFFECT OF FINENESS RATIO ON BOATTAIL DRAG OF CIRCULAR-ARC AFTERBODIES HAVING CLOSURE RATIOS OF 0.50 WITH JET EXHAUST AT MACH NUMBERS UP TO 1.30 ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=393541 By Reubush,David E. Nasa, Washington, D.C. 1973 . 92 , Bound With Nasa Tn D-7190-99

Place Hold on EFFECT OF FINENESS RATIO ON BOATTAIL DRAG OF CIRCULAR-ARC AFTERBODIES HAVING CLOSURE RATIOS OF 0.50 WITH JET EXHAUST AT MACH NUMBERS UP TO 1.30

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=393541 NORMAL-FORCE AND HINGE-MOMENT CHARACTERISTICS AT TRANSONIC SPEEDS OF FLAP-TYPE AILERONS AT THREE SPANWISE LOCATIONS ON A 4-PERCENT-THICK SWEPTBACK-WING-BODY MODEL AND PRESSURE-DISTRIBUTION MEASUREMENN ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=394599 By Runckel,Jack F. Washington NASA Technical report 1961 . 55 , Bound With Nasa Tn D-841-50

Place Hold on NORMAL-FORCE AND HINGE-MOMENT CHARACTERISTICS AT TRANSONIC SPEEDS OF FLAP-TYPE AILERONS AT THREE SPANWISE LOCATIONS ON A 4-PERCENT-THICK SWEPTBACK-WING-BODY MODEL AND PRESSURE-DISTRIBUTION MEASUREMENN

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=394599 INVESTIGATION AT TRANSONIC SPEEDS OF THE LOADING OVER A 45 DEGREE SWEPTBACK WING HAVING AN ASPECT RATIO OF 3, A TAPER RATIO OF 0.2, AND NACA 65A004 AIRFOIL SECTIONS ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=396564 By Runckel,Jack F. Nasa, Washington, D.C. 1961 . 93 , Bound With Nasa Tn D-701-11, 713-20

Place Hold on INVESTIGATION AT TRANSONIC SPEEDS OF THE LOADING OVER A 45 DEGREE SWEPTBACK WING HAVING AN ASPECT RATIO OF 3, A TAPER RATIO OF 0.2, AND NACA 65A004 AIRFOIL SECTIONS

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=396564 INVESTIGATION OF CATALYST BEDS FOR 98-PERCENT-CONCENTRAION HYDROGEN PEROKIDE. ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=399594 By Runckel,Jack F,Willis,Concrad M. Nasa, Washington, D.C. 1963 . 79 , Bound With Nasa Tn D-1801-1807,1809-1810.Lack No-1805

Place Hold on INVESTIGATION OF CATALYST BEDS FOR 98-PERCENT-CONCENTRAION HYDROGEN PEROKIDE.

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=399594 AERODYNAMIC LOAD MEASUREMENTS AND OPENING CHARACTERISTICS OF AUTOMATIC LEADING-EDGE SLATS ON A 45(DEGREE) SWEPTBACK WING AT TRANSONIC SPEEDS ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=401699 By Arabian,Donald D,Runckel,Jack F. Nasa, Washington, D.C. 1961 . 49 , Bound With Nasa Tn D-891-900

Place Hold on AERODYNAMIC LOAD MEASUREMENTS AND OPENING CHARACTERISTICS OF AUTOMATIC LEADING-EDGE SLATS ON A 45(DEGREE) SWEPTBACK WING AT TRANSONIC SPEEDS

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