| Record ID | marc_loc_2016/BooksAll.2016.part06.utf8:172660723:956 |
| Source | Library of Congress |
| Download Link | /show-records/marc_loc_2016/BooksAll.2016.part06.utf8:172660723:956?format=raw |
LEADER: 00956cam a22002651 4500
001 68083459
003 DLC
005 19860401000000.0
008 711124s1967 enkaf b 00010 eng
010 $a 68083459 //r86
015 $aB67-21851
050 0 $aTL507$b.G77 no. 963
082 $a629.132/37
100 10 $aNash, John F.
245 14 $aThe calculation of momentum thickness in a turbulent boundary layer at mach numbers up to unity,$cby J. F. Nash and Miss A. G. Macdonald.
260 0 $aLondon,$bH.M.S.O.,$c1967.
300 $a[1], 24 p.$b9 plates (diagrs.).$c30 cm.
350 $a6/6
490 1 $aAeronautical Research council. Current papers, no. 963
504 $aBibliography: p. 22-24.
650 0 $aTurbulent boundary layer.
650 0 $aAerodynamic load.
650 0 $aAerodynamics, Transonic.
700 10 $aMacdonald, Amelia Gillian Jean,$ejoint author.
830 0 $aCurrent papers (Aeronautical Research Council (Great Britain)) ;$vno. 963.