<![CDATA[PKK Library Search for 'au:"Mangler,K. W."']]>

<![CDATA[PKK Library Search for 'au:"Mangler,K. W."']]> /cgi-bin/koha/opac-search.pl?q=ccl=au%3A%22Mangler%2CK.%20W.%22&format=rss2 5 0 200 SYSTEMS OF COORDINATES SUITABLE FOR THE NUMERICAL CALCULATION OF THREE-DIMENTIONAL FLOW FIELDS ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=392588 By Mangler,K. W.. Her Majestys Stationery Office, London 1975 . 68 , Bound With: Arc Cp 1321-1330

Place Hold on SYSTEMS OF COORDINATES SUITABLE FOR THE NUMERICAL CALCULATION OF THREE-DIMENTIONAL FLOW FIELDS

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=392588 THE INDUCED VELOCITY FIELD OF A ROTOR ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=397105 By Mangler,K W. Her Majesty'S Stationery Office, London 1953 . 16 , Bound With Arc R&M 2613,2622,2783,2637,2695

Place Hold on THE INDUCED VELOCITY FIELD OF A ROTOR

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=397105 USE OF CONICAL CAMBER TO PRODUCE FLOW ATTACHMENT AT THE LEADING EDGE OF A DELTA WING AND TO MINIMIZE LIFT-DEPENDENT DRAG AT SONIC AND SUPERSONIC SPEEDS ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=399876 By Smith,J H.B.,Mangler,K W. Her Majesty'S Stationery Office,London 1963 . 32 , Bound With Arc R&M3271-88,3290

Place Hold on USE OF CONICAL CAMBER TO PRODUCE FLOW ATTACHMENT AT THE LEADING EDGE OF A DELTA WING AND TO MINIMIZE LIFT-DEPENDENT DRAG AT SONIC AND SUPERSONIC SPEEDS

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=399876 CALCULATION OF THE LOAD DISTRIBUTION OVER A WING WITH ARBITRARY CAMBER AND TWIST AT SONIC SPEED ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=402252 By Mangler,K W,Nat,Sc. Her Majesty'S Stationery Office,London 1955 . 46 , Bound With Arc R&M3101,3103-20

Place Hold on CALCULATION OF THE LOAD DISTRIBUTION OVER A WING WITH ARBITRARY CAMBER AND TWIST AT SONIC SPEED

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=402252 CALCULATION OF THE PRESSURE DISTRIBUTION OVER A WING AT SONIC SPEEDS ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=404511 By Mangler,K W. Her Majesty'S Stationery Office, London 1955 . 55 , Bound With Arc R&M2881-87,2889-99 Lack No.2884,2890-94,2896

Place Hold on CALCULATION OF THE PRESSURE DISTRIBUTION OVER A WING AT SONIC SPEEDS

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