| Record ID | marc_loc_2016/BooksAll.2016.part07.utf8:60710551:915 |
| Source | Library of Congress |
| Download Link | /show-records/marc_loc_2016/BooksAll.2016.part07.utf8:60710551:915?format=raw |
LEADER: 00915cam a2200277 4500
001 70853084
003 DLC
005 19881027000000.0
008 711028s1969 enkf b 00010 eng
010 $a 70853084 //r882
015 $aB69-20088
020 $a0114701741
050 0 $aTL507$b.G77 no. 1047$aTL574.A4
082 $a629.13/008 s
100 10 $aSells, C. C. L.$q(Christopher Cedric Lytton)
245 10 $aDesign of a symmetrical section with specified pressure distribution,$cby C. C. L. Sells.
260 0 $aLondon,$bH.M.S.O.,$c1969.
300 $a[1], 11 p., 6 plates.$c30 cm.
350 $a5/6
490 1 $aAeronautical Research Council. Current papers, no. 1047
500 $aCover title.
504 $aBibliography: p. 11.
650 0 $aAerofoils.
650 0 $aLift (Aerodynamics)
650 0 $aAerodynamic load.
830 0 $aCurrent papers (Aeronautical Research Council (Great Britain)) ;$vno. 1047.