LEADER 01978nam 2200577 a 450 001 9910781701003321 005 20230421050703.0 010 $a1-60086-812-6 010 $a1-60086-811-8 035 $a(CKB)2550000000072712 035 $a(EBL)3111622 035 $a(SSID)ssj0000645121 035 $a(PQKBManifestationID)12248159 035 $a(PQKBTitleCode)TC0000645121 035 $a(PQKBWorkID)10680451 035 $a(PQKB)11405793 035 $a(MiAaPQ)EBC3111622 035 $a(Au-PeEL)EBL3111622 035 $a(CaPaEBR)ebr10516727 035 $a(OCoLC)922979035 035 $a(EXLCZ)992550000000072712 100 $a20120112d1997 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 12$aA case study by Aerospatiale and British Aerospace on the Concorde$b[electronic resource] /$fby Jean Rech and Clive S. Leyman 210 $a[Reston, Va. $cAmerican Institute of Aeronautics and Astronautics$d1997?] 215 $a1 online resource (105 p.) 225 1 $aAIAA professional study series 300 $aCover title. 311 $a1-56347-308-9 327 $asection 1. Introduction -- section 2. Design objectives -- section 3. Aircraft aerodynamic layout -- section 4. Flying qualities -- section 5. Performance and noise -- section 6. Powerplant aerodynamics. 410 0$aAIAA professional study series. 606 $aConcorde (Jet transports) 606 $aAerodynamics 615 0$aConcorde (Jet transports) 615 0$aAerodynamics. 676 $a629.133/35/0947 700 $aRech$b J$g(Jean)$0504924 701 $aLeyman$b C. S$g(Clive S.)$01479527 712 02$aAerospatiale (Firm) 712 02$aBritish Aerospace (Firm) 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910781701003321 996 $aA case study by Aerospatiale and British Aerospace on the Concorde$93695687 997 $aUNINA