| Record ID | marc_loc_2016/BooksAll.2016.part06.utf8:128728178:1017 |
| Source | Library of Congress |
| Download Link | /show-records/marc_loc_2016/BooksAll.2016.part06.utf8:128728178:1017?format=raw |
LEADER: 01017cam a22002771 4500
001 67108694
003 DLC
005 20050813185016.0
008 800410s1967 enka b f000 0 eng
010 $a 67108694
015 $aB67-16402
035 $a(OCoLC)6189279
040 $aDLC$cTxCM$dUk$dDLC
042 $apremarc
050 00 $aTL526.G7$bA4 no. 3470
100 1 $aHackett, James Ernest.
245 10 $aWind tunnel tests on a streamlined fan-lift nacelle,$cby J. E. Hackett.
260 $aLondon,$bH.M.S.O.,$c1967.
300 $a50 p.$billus., tables, diagrs.
490 1 $aAeronautical Research Council. Reports and memoranda,$vno. 3470
500 $aCover title.
504 $aBibliography: p. 20-21.
505 0 $aTests on nacelle alone and with wings or underfins fitted.--The effect of forward speed on the lift produced by a lifting fan and its inlet.
650 0 $aAirplanes$xNacelles.
650 0 $aLift fans.
830 0 $aReports and memoranda (Aeronautical Research Council (Great Britain)) ;$vno. 3470.