<![CDATA[PKK Library Search for 'au:"Miles,C.J.W"']]>

<![CDATA[PKK Library Search for 'au:"Miles,C.J.W"']]> /cgi-bin/koha/opac-search.pl?q=ccl=au%3A%22Miles%2CC.J.W%22&format=rss2 4 0 200 MEASUREMENTS OF PITCHING OSCILLATION DERIVATIVES AT SUBSONIC AND TRANSONIC SPEEDS FOR A CROPPED DELT WING OF ASPECT RATIO 1.8 (INTERIM REPORT). ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=395459 By Miles,C.J.W,Bratt,J B. Her Majesty'S Stationery Office, London 1961 . 5 , Bounds With Arc C.P. 531-33, 535-40

Place Hold on MEASUREMENTS OF PITCHING OSCILLATION DERIVATIVES AT SUBSONIC AND TRANSONIC SPEEDS FOR A CROPPED DELT WING OF ASPECT RATIO 1.8 (INTERIM REPORT).

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=395459 MEASUREMENTS OF DIRECT PITCHING OSCILLATION DERIVATIVES FOR THREE CROPPED DELTA AND THREE ARROWHEAD PLANFORMS AT SUBSONIC AND TRANSONIC SPEEDS. ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=396122 By Miles,C.J.W. Her Majesty'S Stationery Office, London 1965 . 30 , Bound With Arc R&M3381-95, 3398-99 Lack No.3387, 3390-91, 3394 And 3396

Place Hold on MEASUREMENTS OF DIRECT PITCHING OSCILLATION DERIVATIVES FOR THREE CROPPED DELTA AND THREE ARROWHEAD PLANFORMS AT SUBSONIC AND TRANSONIC SPEEDS.

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=396122 MEASUREMENTS THE DIRECT HINGS-MOMENT DERIVATIVES AT SUBSONIC AND TRANSONIC SPEEDS FOR A CROPPED DELTA WING WITH OSCILLATING FLAP. ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=403711 By Bratt,J B,Miles,C.J W. Her Majesty'S Stationery Office,London 1957 . 22 , Bound With Arc R&M-3161-3162,3164-3170.

Place Hold on MEASUREMENTS THE DIRECT HINGS-MOMENT DERIVATIVES AT SUBSONIC AND TRANSONIC SPEEDS FOR A CROPPED DELTA WING WITH OSCILLATING FLAP.

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=403711 EXPERIMENTS IN THE COMPRESSED AIR TUNNEL ON SWEPT-BACK WINGS INCLUDING TWO DELTA WINGS ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=404597 By Jones,R,Miles,C J W. Her Majesty'S Stationery Office, London 1954 . 26 , Bound With Arc R&M 2861-70,2872-80lack No.2862,2868,2873

Place Hold on EXPERIMENTS IN THE COMPRESSED AIR TUNNEL ON SWEPT-BACK WINGS INCLUDING TWO DELTA WINGS

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