LEADER 00852nam0-2200313---450- 001 990008760230403321 005 20090903132230.0 010 $a0-246-11914-4 035 $a000876023 035 $aFED01000876023 035 $a(Aleph)000876023FED01 035 $a000876023 100 $a20081119d1982----km-y0itay50------ba 101 0 $aeng 102 $aGB 105 $aa-------001yy 200 1 $a<>microlight flying manual$fR.D. Campbell and J. Jones 210 $aLondon$cAviation training$d1982 215 $a1 v.$cill.$d25 cm 300 $aPaginazione varia 700 1$aCampbell,$bRonald D.$0316032 701 1$aJones,$bJohn$0352404 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990008760230403321 952 $aT6$b55$fDINPA 959 $aDINPA 996 $aMicrolight flying manual$9810589 997 $aUNINA LEADER 01250cam0-2200373---450- 001 990008676250403321 005 20110118130702.0 010 $a91-85194-22-0 035 $a000867625 035 $aFED01000867625 035 $a(Aleph)000867625FED01 035 $a000867625 100 $a20080620e19811950km-y0itay50------ba 101 0 $aeng 102 $aSE 105 $aa-------001yy 200 1 $aGunnar Asplund architect 1885-1940$eplans sketches and photographs$fpublished by Svenska Arkitekters Riksförbund$gedited by Gustav Holmdahl, Sven Ivar Lind, Kjell Ödeen$gwith an essay by Hakon Ahlberg 210 $aStockholm$cByggförlaget$d1981 215 $a240 p.$cill.$d27 cm 300 $aRipr. facs. dell'ed.: Stockholm : Ab Tidskriften Byggmästaren, 1950 517 1 $aGunnar Asplund architect 610 0 $aAsplund, Gunnar$aDisegni architettonici 700 1$aAsplund,$bErik Gunnar$035819 702 1$aAhlberg,$bHakon 702 1$aHolmdahl,$bGustav 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990008676250403321 952 $a10.655$b2313$fDARST 952 $aI(FN) A 52$b2712$fDCATA 959 $aDARST 959 $aDCATA 996 $aGunnar Asplund architect 1885-1940$9717055 997 $aUNINA LEADER 02299nam 2200517 450 001 9910706576003321 005 20171120092821.0 035 $a(CKB)5470000002456685 035 $a(OCoLC)1012398455 035 $a(EXLCZ)995470000002456685 100 $a20171120j200102 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aComputational analysis of the combustion process in an axisymmetric,RBCC flowpath /$fChristopher J. Steffen, Shaye Yungster 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dFebruary 2001. 215 $a1 online resource (15 pages) $cillustrations 225 1 $aNASA/TM ;$v2001-210679 300 $a"February 2001." 300 $a"Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting cosponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000." 300 $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page. 320 $aIncludes bibliographical references (page 15). 517 3 $aComputational analysis of the combustion processes in an axisymmetric, rocket based combined cycle flowpath 606 $aComputational fluid dynamics$2nasat 606 $aNumerical analysis$2nasat 606 $aCombustion physics$2nasat 606 $aThree dimensional models$2nasat 606 $aSupersonic combustion ramjet engines$2nasat 606 $aSimulation$2nasat 615 7$aComputational fluid dynamics. 615 7$aNumerical analysis. 615 7$aCombustion physics. 615 7$aThree dimensional models. 615 7$aSupersonic combustion ramjet engines. 615 7$aSimulation. 700 $aSteffen$b Christopher J.$01386995 702 $aYungster$b Shaye 712 02$aNASA Glenn Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910706576003321 996 $aComputational analysis of the combustion process in an axisymmetric,RBCC flowpath$93436394 997 $aUNINA