LEADER 01631nam a2200325 i 4500 001 991001064509707536 008 050614m19871991it a 000 0 ita d 020 $a8820319845 (v.2) 020 $a8820315157 (v.1) 035 $ab13315146-39ule_inst 040 $aDip.to Ingegneria dell'Innovazione$bita 082 0 $a624.151$221 100 1 $aCestelli Guidi, Carlo$0426 245 10$aGeotecnica e tecnica delle fondazioni /$cCarlo Cestelli Guidi 250 $a8. ed. riveduta e aggiornata 260 $aMilano :$bHoepli,$c1987- 300 $av. :$bill. ;$c25 cm 505 1 $gV.1. parte1 :$tPrincipi di meccanica del terreno 505 1 $gV.1. parte2 :$tTeoria di meccanica del terreno 505 1 $gV.2 :$tTecnica delle fondazioni 650 4$aGeotecnics 907 $a.b13315146$b07-01-14$c31-05-05 912 $a991001064509707536 945 $aLE026 624.151 D GUI 01.01 V.I C.1 1987 $cV.I$g1$i2026000016504$lle026$nProf. Aiello, Ombres / Biblioteca$op$pE78.20$q-$rn$s- $t1$u4$v0$w4$x0$y.i14115761$z28-07-05 945 $aLE026 624.151 D GUI 01.01 V.I C.2 1987$cV.I$g1$i2026000016498$lle026$nProf. Aiello, Ombres / Biblioteca$op$pE78.20$q-$rl$s- $t0$u23$v2$w23$x0$y.i14115773$z28-07-05 945 $aLE026 624.151 D GUI 01.01 V.II 1991$cV. II$g1$i2026000024103$lle026$nBiblioteca$op$pE106.00$q-$rn$s- $t1$u11$v0$w11$x0$y.i1412239x$z07-09-05 945 $aLE016 624.151 CES 01.02$cVol.2$g1$i2016000113761$lle016$on$pE106.00$q-$rn$so $t0$u0$v0$w0$x0$y.i14791389$z02-07-08 996 $aGeotecnica e tecnica delle fondazioni$943190 997 $aUNISALENTO 998 $ale026$ale016$b14-06-05$cm$da $e-$fita$git $h0$i0 LEADER 02022nam 2200577 450 001 9910706143703321 005 20170906140120.0 035 $a(CKB)5470000002454991 035 $a(OCoLC)1003045325 035 $a(EXLCZ)995470000002454991 100 $a20170906j199912 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aNacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds /$fRobert J. Mack 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dDecember 1999. 215 $a1 online resource (15 pages) $cillustrations 225 1 $aNASA/TM ;$v1999-209534 300 $a"December 1999." 300 $a"Performing organization: NASA Langley Research Center"--Report documentation page. 320 $aIncludes bibliographical references (pages 13-15). 606 $aAerodynamic characteristics$2nasat 606 $aBody-wing configurations$2nasat 606 $aNacelles$2nasat 606 $aSonic booms$2nasat 606 $aWings$2nasat 606 $aAerodynamic configurations$2nasat 606 $aSupersonic flight$2nasat 606 $aAerodynamic noise$2nasat 606 $aNoise reduction$2nasat 606 $aWind tunnel tests$2nasat 615 7$aAerodynamic characteristics. 615 7$aBody-wing configurations. 615 7$aNacelles. 615 7$aSonic booms. 615 7$aWings. 615 7$aAerodynamic configurations. 615 7$aSupersonic flight. 615 7$aAerodynamic noise. 615 7$aNoise reduction. 615 7$aWind tunnel tests. 700 $aMack$b Robert J.$01408827 712 02$aLangley Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910706143703321 996 $aNacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds$93512804 997 $aUNINA