| Record ID | marc_loc_2016/BooksAll.2016.part06.utf8:116110226:905 |
| Source | Library of Congress |
| Download Link | /show-records/marc_loc_2016/BooksAll.2016.part06.utf8:116110226:905?format=raw |
LEADER: 00905cam a2200253 4500
001 67078700
003 DLC
005 19860327000000.0
008 731001s1967 enkaf b 00010 eng
010 $a 67078700 //r86
015 $aB67-3000
050 0 $aTL507$b.G77 no. 890
082 $a629.132/37
100 10 $aPeake, D. J.
245 14 $aThe use of air injection to prevent separation of the turbulent boundary layer in supersonic flow,$cby D. J. Peake.
260 0 $aLondon,$bH.M.S.O.,$c1966 [i.e. 1967]
300 $a30 p.$b20 plates (incl. diagrs.), tables.$c33 cm.
490 1 $a[Great Britain] Aeronautical Research Council. Current papers$vno. 890
504 $aBibliography: p. 18-20.
650 0 $aBoundary layer control.
650 0 $aAir jets.
650 0 $aTurbulence.
650 0 $aAerodynamics, Supersonic.
830 0 $aCurrent papers (Aeronautical Research Council (Great Britain)) ;$vno. 890.