<![CDATA[PKK Library Search for 'au:"Goldberg, Theodore J."']]>

<![CDATA[PKK Library Search for 'au:"Goldberg, Theodore J."']]> /cgi-bin/koha/opac-search.pl?q=ccl=au%3A%22Goldberg%2C%20Theodore%20J.%22&format=rss2 6 0 200 NASA Technical Note [NASA TN D-2550]: Application of generalized Newtonian theory to three-dimensional sharp-nose shock-detached bodies at mach for angles of attack up to 25 [degree] ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=394103 Washington NASA 1965 . 41p , Bound together NASA TN D-2541 to 2550 | Bound vol. Acc. No. 67642 contains Acc. No. TR9902 to TR9910

Place Hold on NASA Technical Note [NASA TN D-2550]: Application of generalized Newtonian theory to three-dimensional sharp-nose shock-detached bodies at mach for angles of attack up to 25 [degree]

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=394103 EFFECTS OF ROUNDING CORNERS AND LEADING EDGES ON THE WINDWARD-SURFACE PRESSURE OF A DELTA WING SWEPT 65(DG) AT A MACH NUMBER OF 5.96 AT ANGLES OF ATTACK FROM 65(DG) TO 115(DG)AND ANGLES OF ROLL FROM.. ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=394384 By Goldberg,Theodore J. Nasa, Washington, D.C. 1963 . 34 , Bound With Nasa Tn D-1951-1960

Place Hold on EFFECTS OF ROUNDING CORNERS AND LEADING EDGES ON THE WINDWARD-SURFACE PRESSURE OF A DELTA WING SWEPT 65(DG) AT A MACH NUMBER OF 5.96 AT ANGLES OF ATTACK FROM 65(DG) TO 115(DG)AND ANGLES OF ROLL FROM..

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=394384 CENTER-LINE PRESSURE DISTRIBUTIONS ON TWO-DIMENSIONAL BODIES WITH LEADING-EDGE ANGLES GREATER THAN THAT FOR SHOCK DETACHMENT AT MACH NUMBER 6 AND ANGLES OF ATTACK UPTO 25(DEGREE) ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=394517 By Goldberg,Theodore J, Ashby,George C. Nasa, Washington, D.C. 1963 . 53 , Bound With Nasa Tn D-1791-95

Place Hold on CENTER-LINE PRESSURE DISTRIBUTIONS ON TWO-DIMENSIONAL BODIES WITH LEADING-EDGE ANGLES GREATER THAN THAT FOR SHOCK DETACHMENT AT MACH NUMBER 6 AND ANGLES OF ATTACK UPTO 25(DEGREE)

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=394517 AFTERBODY PRESSURES ON TWO-DIMENSIONAL BOATTAILED BODIES HAVING TURBULENT BOUNDARY LAYERS AT MACH 56.98 ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=398780 By Staylor,W Frank. Nasa, Washington, D.C. 1964 . 36 , Bound With Nasa Tn D-2341-49.

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]]> /cgi-bin/koha/opac-detail.pl?biblionumber=398780 HYPERSONIC AERODYNAMIC CHARACTERISTICS OF TWO DELTA-WING X-15 AIRPLANE CONFIGURATIONS ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=400126 By Goldberg,Theodore J. Nasa, Washington, D.C. 1969 . 102 , Bound With Nasa Tn D-5491-97 Lack No.5494,5496

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]]> /cgi-bin/koha/opac-detail.pl?biblionumber=400126 INVESTIGATION ON THE USE OF A FREELY ROTATING ROTOR AT THE COWL FACE OF A SUPERSONIC CONICAL INLET TO REDUCE INLET FLOW DISTORTION ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=402221 By Goldberg,Theodore J. Nasa, Washington, D.C. 1959 , Bound With Nasa Memo 5-12-59l-5-26-59l Lack No.14-17, 19, 21-22, 27

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