| Record ID | marc_records_scriblio_net/part10.dat:73280870:891 |
| Source | Scriblio |
| Download Link | /show-records/marc_records_scriblio_net/part10.dat:73280870:891?format=raw |
LEADER: 00891cam 2200253 4500
001 77433302 //r862
003 DLC
005 19860401000000.0
008 700112s1968 enkaf b 00010 eng
010 $a 77433302 //r862
015 $aB68-20712
050 0 $aTL507$b.G77 no. 991
082 $a629.13/008 s
100 10 $aFirmin, Michael Charles Peter,$d1929-
245 14 $aThe pressure distribution at zero lift on a slender delta wing at transonic speeds,$cby M. C. P. Firmin.
260 0 $aLondon,$bH.M.S.O.,$c1968.
300 $a[1], 10 p.$b2 plates, illus.$c30 cm.
350 $a6/6
490 1 $aAeronautical Research Council. Current papers, no. 991
504 $aBibliography: p. 10.
650 0 $aAerodynamics, Transonic.
650 0 $aAirplanes$xWings, Triangular.
650 0 $aAerodynamic load.
830 0 $aCurrent papers (Aeronautical Research Council (Great Britain)) ;$vno. 991.