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100   $a20110623d1987----km-y0itay50------ba
101 0 $aeng
102   $aUS
105   $aa---j---001yy
200 1 $aFundamental techniques in veterinary surgery$fCharles D. Knecht ... [et. al.]
205   $a3rd ed
210   $aPhiladelphia$cW. B. Saunders company$d1987
215   $aXVI, 349 p.$cill.$d27 cm
453  0$1001000863121
610 0 $aChirurgia veterinaria$aManuali
676   $a636.089
700  1$aKnecht,$bCharles D.$0306892
801  0$aIT$bUNINA$gRICA$2UNIMARC
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996   $aFundamental techniques in veterinary surgery$9762827
997   $aUNINA

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100   $a20130526j199801    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aWind-tunnel evaluation of the effect of blade nonstructural mass distribution on helicopter fixed-system loads /$fMatthew L. Wilbur [and four others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJanuary 1998.
215   $a1 online resource (247 pages) $cillustrations
225 1 $aNASA/TM ;$v1998-206281
225 1 $aARL-TR ;$v1401
300   $aTitle from title screen (viewed Aug. 3, 2016).
300   $a"January 1998."
300   $a"Performing organization: Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 5).
606   $aHelicopters$2nasat
606   $aLoads (forces)$2nasat
606   $aRotary wing aircraft$2nasat
606   $aRotor dynamics$2nasat
606   $aWind tunnel tests$2nasat
615  7$aHelicopters.
615  7$aLoads (forces)
615  7$aRotary wing aircraft.
615  7$aRotor dynamics.
615  7$aWind tunnel tests.
700   $aWilbur$b Matthew L.$01389368
712 02$aLangley Research Center,
712 02$aVehicle Technology Center (U.S. Army Research Laboratory),
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