| Record ID | marc_loc_2016/BooksAll.2016.part06.utf8:122580245:890 |
| Source | Library of Congress |
| Download Link | /show-records/marc_loc_2016/BooksAll.2016.part06.utf8:122580245:890?format=raw |
LEADER: 00890cam a2200229 4500
001 67093711
003 DLC
005 19860326000000.0
008 731001s1966 enkaf b 00010 eng
010 $a 67093711 //r86
015 $aB67-808
050 0 $aTL507$b.G77 no. 861
082 $a621.43/3
100 10 $aJohnston, I. H.
245 10 $aFurther tests on a three-stage turbine of low reaction to examine the effects of reduced rotor pitch and improved sealing,$cby I. H. Johnston and D. C. Dransfield.
260 0 $aLondon,$bH.M.S.O.,$c1966.
300 $a[1], 15 p.$b13 plates (diagrs.) tables.$c33 cm.
490 1 $a[Great Britain] Aeronautical Research Council. Current papers$vno. 861
504 $aBibliography: p. 15.
650 0 $aGas-turbines$xTesting.
700 10 $aDransfield, D. C.,$ejoint author.
830 0 $aCurrent papers (Aeronautical Research Council (Great Britain)) ;$vno. 861.