<![CDATA[PKK Library Search for 'au:"Clarence A Brown"']]>

<![CDATA[PKK Library Search for 'au:"Clarence A Brown"']]> /cgi-bin/koha/opac-search.pl?q=ccl=au%3A%22Clarence%20A%20Brown%22&format=rss2 4 0 200 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 Evaluation of flow properties behind 120 degree and 140 degree included angle cones and a viking 75 entry vehicle at mach numbers from 1.60 to 3.95 ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=396517 By Brown, Clarence A.. Washington, D.C. National Aeronautics and Space Administration 1973 . 100p

Place Hold on Evaluation of flow properties behind 120 degree and 140 degree included angle cones and a viking 75 entry vehicle at mach numbers from 1.60 to 3.95

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=396517 Flight test performance and description of a rocket vehicle for producing low speed artificial meteors. ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=406325 By Clarence A Brown.

Place Hold on Flight test performance and description of a rocket vehicle for producing low speed artificial meteors.

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=406325 Effects of reynolds number and model support on the supersonic aerodynamic characteristics of a 140 degree included angle cone [NASA TM X-3019] ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=563670 By Trescot, Charles D.. Washington, D.C. National Aeronautics and Space Administration 1974 . 72p

Place Hold on Effects of reynolds number and model support on the supersonic aerodynamic characteristics of a 140 degree included angle cone [NASA TM X-3019]

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