| Record ID | marc_loc_2016/BooksAll.2016.part08.utf8:81044854:1016 |
| Source | Library of Congress |
| Download Link | /show-records/marc_loc_2016/BooksAll.2016.part08.utf8:81044854:1016?format=raw |
LEADER: 01016cam a2200229 4500
001 73490390
003 DLC
005 20130418083032.0
008 701009s1966 at a b 000 0 eng
010 $a 73490390
040 $aDLC$cDLC$dDLC
050 00 $aTL507$b.A8 no. 69
100 1 $aChan, Y. Y.
245 10 $aPressure distributions on planar and cruciform delta wings attached to cylindrical bodies in supersonic flow;$bpart 1-theoretical results for the wing thickness case,$cby Y. Y. Chan and L. M. Sheppard.
260 $a[Melbourne]$bDept. of Supply, Australian Aeronautical Research Committee,$c1966.
300 $a82 p.$billus.$c28 cm.
490 1 $aDept. of Supply. Australian Aeronautical Research Committee. Report ACA-69
504 $aIncludes bibliographical references.
650 0 $aAirplanes$xWings, Triangular.
650 0 $aAerodynamics, Supersonic.
700 1 $aSheppard, L. M.,$ejoint author.
810 1 $aAustralia.$bDepartment of Supply.$bAeronautical Research Consultative Committee.$tReport ACA$v69