| Record ID | marc_loc_2016/BooksAll.2016.part06.utf8:112942307:1067 |
| Source | Library of Congress |
| Download Link | /show-records/marc_loc_2016/BooksAll.2016.part06.utf8:112942307:1067?format=raw |
LEADER: 01067cam a22003011 4500
001 67071453
003 DLC
005 20050509183955.0
008 800410s1966 enka b f000 0 eng
010 $a 67071453
015 $aB66-23860
035 $a(OCoLC)6188134
040 $aDLC$cTxCM$dDLC
042 $apremarc
050 00 $aTL526.G7$bA4 no. 3426
100 1 $aTaylor, A. S.
245 10 $aEffects of longitudinal elastic camber on slender aircraft in steady symmetrical flight;$bParts I and II,$cby A. S. Taylor and W. F. W. Urich.
260 $aLondon,$bH.M.S.O.,$c1966.
300 $a95 p.$bdiagrs.
490 1 $aAeronautical Research Council (Great Britain) Reports and memoranda,$vno. 3426
500 $aCover title.
504 $aIncludes bibliographies.
650 0 $aAeroelasticity.
650 0 $aAirplanes$xHandling characteristics.
650 0 $aCamber (Aerofoils)
650 0 $aSupersonic transport planes.
700 1 $aUrich, W. F. W.,$ejoint author.
830 0 $aReports and memoranda (Aeronautical Research Council (Great Britain)) ;$vno. 3426.