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

<![CDATA[PKK Library Search for 'au:"Walkden,F"']]> /cgi-bin/koha/opac-search.pl?q=ccl=au%3A%22Walkden%2CF%22&format=rss2 3 0 200 FORM OF THE SUPERSONIC FLOW EQUATIONS FOR AN IDEAL GAS ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=392150 By Walkden, F.. , Bound With: R&M 3749-3759

Place Hold on FORM OF THE SUPERSONIC FLOW EQUATIONS FOR AN IDEAL GAS

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=392150 THE EQUATIONS MOTION OF A VISCOUS COMPRESSIBLE GAS REFERRED TO AN ARBITRARILY MOVING CO-ORDINATE SYSTEM ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=396813 By Walkden,F. Her Majesty'S Stationery Office, London 1966 . 23 , Bound With Arc R&M-3600-3608.3610-3612.Lack No-3602,3606,3607.

Place Hold on THE EQUATIONS MOTION OF A VISCOUS COMPRESSIBLE GAS REFERRED TO AN ARBITRARILY MOVING CO-ORDINATE SYSTEM

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=396813 A NUMERICAL METHOD FOR CALCULATING THE PRESSURE DUE TO THICKNESS ON SYMMETRICAL WINGS AT ZERO INCIDENCE IN SUPERSONIC FLOW ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=401053 By Eldridge,R H. Her Majesty'S Stationery Office, London 1968 . 49 , Bound With Arc R&M3533,3542-49 Lack No.3534,3536-41,3547

Place Hold on A NUMERICAL METHOD FOR CALCULATING THE PRESSURE DUE TO THICKNESS ON SYMMETRICAL WINGS AT ZERO INCIDENCE IN SUPERSONIC FLOW

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