LEADER 01099nam0-2200301---450- 001 990008408040403321 005 20061026112454.0 035 $a000840804 035 $aFED01000840804 035 $a(Aleph)000840804FED01 035 $a000840804 100 $a20061026d1947----km-y0itay50------ba 101 0 $aeng 102 $aGB 105 $aaf------001yy 200 1 $a<>effect of spanwise rib-boom stiffness on the stress distribution near a wing cut-out$fby E. H. Mansfield 210 $aLondon$c[s.n.]$d1947 215 $a16 p., [9] p. di tav.$cill.$d33 cm 225 1 $aReports and memoranda$fAeronautical Research Council, London. Procurement Executive, Ministry of Defense$v2663 300 $aIn testa al front.: Royal Aircraft establishment, Farnborough. - Report Structures 13 700 1$aMansfield,$bEric Harold$0298597 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990008408040403321 952 $aA 39$fDINPA 959 $aDINPA 996 $aEffect of spanwise rib-boom stiffness on the stress distribution near a wing cut-out$9725224 997 $aUNINA