LEADER 05509nam 2200697 450 001 9910464871403321 005 20200520144314.0 010 $a0-12-419977-1 035 $a(CKB)3710000000087729 035 $a(EBL)1637338 035 $a(SSID)ssj0001154707 035 $a(PQKBManifestationID)11753983 035 $a(PQKBTitleCode)TC0001154707 035 $a(PQKBWorkID)11163376 035 $a(PQKB)11242970 035 $a(MiAaPQ)EBC1637338 035 $a(CaSebORM)9780124199538 035 $a(PPN)192786733 035 $a(Au-PeEL)EBL1637338 035 $a(CaPaEBR)ebr10839253 035 $a(CaONFJC)MIL604990 035 $a(OCoLC)871224213 035 $a(EXLCZ)993710000000087729 100 $a20140306h20142014 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aCommercial airplane design principles /$fPasquale M. Sforza 205 $a1st edition 210 1$aOxford, [England] ;$aWaltham, [Massachusetts] :$cButterworth-Heinemann,$d2014. 210 4$dİ2014 215 $a1 online resource (623 p.) 225 0 $aElsevier aerospace engineering series Commercial airplane design principles 300 $aDescription based upon print version of record. 311 $a0-12-419953-4 320 $aIncludes bibliographical references and index. 327 $aHalf Title; Title Page; Copyright; Contents; Preface; Introduction and Outline of an Airplane Design Report; 1 Market Survey and Mission Specification; 1.1 A growing market for commercial aircraft; 1.2 Technology drivers; 1.2.1 Fuel efficiency; 1.2.2 Weight reduction; 1.2.3 Drag reduction; 1.2.4 Engine design; 1.2.5 Carbon footprint; 1.2.6 Biofuels; 1.2.7 Alternative fuels and power sources; 1.2.8 Noise and vibration; 1.3 Cargo aircraft; 1.4 Design summary; 1.4.1 Mission specification; 1.4.2 The market survey; References; 2 Preliminary Weight Estimation; 2.1 The mission specification 327 $a2.2 The mission profile2.3 Weight components; 2.3.1 Gross, takeoff, and operating empty weights; 2.3.2 Passenger and crew weights; 2.3.3 Cargo weight; 2.3.4 Fuel weight; 2.3.5 Fuel consumption by mission segment; 2.3.6 Fuel consumption in segments other than cruise; 2.3.7 Fuel consumption in cruise; 2.3.8 Selection of cruise performance characteristics; 2.4 Empty weight trends; 2.5 Fuel characteristics; 2.6 Estimation of the takeoff and empty weights; 2.6.1 New materials for weight reduction; 2.7 Weight estimation for turboprop-powered aircraft 327 $a2.7.1 Fuel weight estimation for turboprop airliners2.7.2 Empty weight estimation for turboprop airliners; 2.8 Design summary; 2.9 Nomenclature; 2.9.1 Subscript; References; 3 Fuselage Design; 3.1 Introduction; 3.2 Commercial aircraft cabin volume and pressure; 3.2.1 Cabin volume; 3.2.2 Cabin pressure; 3.3 General cabin layout; 3.4 Cabin cross-section; 3.5 Estimation of fuselage width; 3.6 Estimation of fuselage length; 3.7 Influence of fuselage fineness ratio; 3.7.1 Fuselage effects on drag; 3.7.2 Fuselage effect on lift; 3.8 Estimation of nose cone and tail cone length; 3.9 Cargo containers 327 $a3.10 Emergency exits3.11 Recent developments in fuselage design; 3.12 Design summary; References; 4 Engine Selection; 4.1 Introduction; 4.2 Landing requirements; 4.3 Wing loading in landing; 4.4 Landing field length; 4.5 Wing loading in takeoff; 4.6 Takeoff distance; 4.7 Cruise requirements; 4.8 Construction of the engine selection design chart; 4.9 Flight test data for landing and power approach; 4.10 Turbojet and turbofan engines; 4.10.1 Dual shaft turbojet; 4.10.2 Dual shaft high bypass turbofan; 4.10.3 Determination of net thrust; 4.10.4 Net thrust in takeoff; 4.10.5 Net thrust in cruise 327 $a4.10.6 Specific fuel consumption in cruise4.11 Turboprops; 4.11.1 Takeoff distance; 4.11.2 Turboprop cruise requirements; 4.11.3 Estimating takeoff thrust and specific fuel consumption; 4.12 Engine-out operation and balanced field length; 4.13 Design summary; 4.14 Nomenclature; References; 5 Wing Design; 5.1 General wing planform characteristics; 5.1.1 The straight-tapered wing planform; 5.1.2 Cranked wing planform; 5.1.3 Wing dihedral; 5.2 General airfoil characteristics; 5.2.1 Airfoil sections; 5.2.2 Airfoils at angle of attack; 5.2.3 Airfoil selection 327 $a5.2.4 Compressibility effects on airfoils 330 $a Commercial Airplane Design Principles is a succinct, focused text covering all the information required at the preliminary stage of aircraft design: initial sizing and weight estimation, fuselage design, engine selection, aerodynamic analysis, stability and control, drag estimation, performance analysis, and economic analysis. The text places emphasis on making informed choices from an array of competing options, and developing the confidence to do so. Shows the use of standard, empirical, and classical methods in support of the design process Exp 606 $aAirplanes$xDesign and construction 606 $aAerospace engineering 606 $aAircraft industry 608 $aElectronic books. 615 0$aAirplanes$xDesign and construction. 615 0$aAerospace engineering. 615 0$aAircraft industry. 676 $a629.1341 700 $aSforza$b P. M$0952888 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910464871403321 996 $aCommercial airplane design principles$92154336 997 $aUNINA