<![CDATA[PKK Library Search for 'au:"Putnam, Lawrence E."']]>

<![CDATA[PKK Library Search for 'au:"Putnam, Lawrence E."']]> /cgi-bin/koha/opac-search.pl?q=ccl=au%3A%22Putnam%2C%20Lawrence%20E.%22&format=rss2 7 0 200 EXPERIMENTAL DETERMINATION OF EQUIVALENT SOLID BODIES TO REPRESENT JETS EXHAUSTING INTO A MACH 2.20 EXTERNAL STREAM ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=393798 By Putnam,Lawrence E. Nasa, Washington, D.C. 1969 . 66 , Bound With Nasa Tn D-5550-69

Place Hold on EXPERIMENTAL DETERMINATION OF EQUIVALENT SOLID BODIES TO REPRESENT JETS EXHAUSTING INTO A MACH 2.20 EXTERNAL STREAM

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=393798 STATIC AERODYNAMIC CHARACTERISTIC OF A THREE -STAGE ROCKET VEHICLE HAVING VARIOUS FIN CONFIGURATIONS AT LOW SUBSONIC MACH NUMBERS AND ANGLES OF ATTACK UP TO 28(DEGREE) ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=394670 By Brown,Clarence A.. NASA, Washington, D.C. 1963 . 26p , Technical Reports D-1781 Bound Vol. No.101074; TR8292-99

Place Hold on STATIC AERODYNAMIC CHARACTERISTIC OF A THREE -STAGE ROCKET VEHICLE HAVING VARIOUS FIN CONFIGURATIONS AT LOW SUBSONIC MACH NUMBERS AND ANGLES OF ATTACK UP TO 28(DEGREE)

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=394670 FXPLORATORY INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 0.95 OF THE EFFECTS OF JETS BLOWN OVER A WING ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=394961 By Putnam,Lawrence E. Nasa, Washington, D.C. 1973 . 69 , Bound With Nasa Tn D-7360-69

Place Hold on FXPLORATORY INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 0.95 OF THE EFFECTS OF JETS BLOWN OVER A WING

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=394961 NASA Technical Note [NASA TN D-1947]: Transonic investigation of the static longitudinal aerodynamic characteristics of low-aspect-ratio wing-body configurations at angles of attack from 0 [degree] to 90 [degree] ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=396018 Washington NASA 1963 . 36p , Bound together NASA TN D-1941 to 1950 | Bound vol. Acc. No. 65584 contains Acc. No. TR10692 to TR10700

Place Hold on NASA Technical Note [NASA TN D-1947]: Transonic investigation of the static longitudinal aerodynamic characteristics of low-aspect-ratio wing-body configurations at angles of attack from 0 [degree] to 90 [degree]

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=396018 HYPERSONIC AERODYNAMIC CHARACTERISTICS OF WING-BODY CONFIGURATIONS WITH CANARD CONTROLS ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=397343 By Putnam,Lawrence E. Nasa, Washington, D.C. 1966 . 51 , Bound With Nasa Tn D-3721-3727, 3729-3730

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]]> /cgi-bin/koha/opac-detail.pl?biblionumber=397343 AN ANALYTICAL STUDY OF THE EFFECTS OF JETS LOCATED MORE THEN ONE JET DIAMETER ABOVE A WING AT SUBSONIC SPEEDS ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=399663 By Putnam,Lawrence E. Nasa, Washington, D.C. 1974 . 41 , Bound With Nasa Tn D-7742-53,7756-7760 Lack No.7746,7748-7749,7752,7755,7758-7760

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]]> /cgi-bin/koha/opac-detail.pl?biblionumber=399663 EFFECTS OF AFT-FUSELAGE-MOUNTED NACELLES ON THE SUBSONIC LONGITUDINAL AERODYNAMIC CHARACTRISTICS OF A TWIN-TURBOJET AIRPLANE. ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=479563 By PUTNAM,LAWRENCE E. NASA, WASHINGTON, D.C. 1966 . ,54,,,,,, , Bound with NASA TN D-3782-90

Place Hold on EFFECTS OF AFT-FUSELAGE-MOUNTED NACELLES ON THE SUBSONIC LONGITUDINAL AERODYNAMIC CHARACTRISTICS OF A TWIN-TURBOJET AIRPLANE.

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