LEADER 04389nam 2200577 450 001 9910798269903321 005 20230125181742.0 010 $a1-60650-684-6 035 $a(CKB)3710000000610777 035 $a(OCoLC)945180204 035 $a(CaBNvSL)swl00406302 035 $a(MiAaPQ)EBC4432251 035 $a(Au-PeEL)EBL4432251 035 $a(CaPaEBR)ebr11169569 035 $a(CaONFJC)MIL901613 035 $a(OCoLC)945612332 035 $a(EXLCZ)993710000000610777 100 $a20190123d2018 uy 0 101 0 $aeng 135 $aurcnu|||||||| 181 $2rdacontent 182 $2rdamedia 183 $2rdacarrier 200 10$aAircraft performance and sizing$hVolume I $efundamentals of aircraft performance /$fTimothy Takahashi 210 1$aNew York, NY :$cMomentum Press,$d[2018] 210 4$dİ2018 215 $a1 online resource (xvi, 230 pages) $cillustrations 225 1 $aAerospace engineering collection 311 $a1-60650-683-8 320 $aIncludes bibliographical references and index. 327 $a1. Introduction -- 1.1 Defining a clean-sheet design -- 1.2 Aircraft purpose, the explicit requirements -- 1.3 Certification, the implied requirements -- 327 $a2. Flight mechanics basics -- 2.1 Reference units -- 2.2 Coordinate frames -- 2.3 Standard atmosphere -- 2.4 How pilots actually fly airplanes -- 327 $a3. Propulsion system design drivers and performance -- 3.1 Gas turbine fundamentals -- 3.2 Calculating thrust and fuel flow -- 3.3 Propulsion system components and design drivers -- 3.4 Example engine performance data -- 327 $a4. Aerodynamic analysis fundamentals: lift and drag -- 4.1 Full configuration drag estimation -- 4.2 Zero-lift drag at incompressible speeds -- 4.3 Zero-lift drag due to compressibility -- 4.4 Drag due to lift at incompressible speeds -- 4.5 Drag due to lift arising from compressibility -- 4.6 "Crud drag," the drag of real versus idealized aerostructures -- 4.7 Maximum lift coefficient/buffet boundary -- 4.8 Angle of attack -- 4.9 Take-off, approach, and landing aerodynamics -- 327 $a5. Kinematic "point-performance" principles -- 5.1 Standard atmosphere revisited -- 5.2 Computing stall speed -- 5.3 Minimum and maximum permissible flight speeds -- 5.4 The energy-maneuverability skymap plot -- 5.5 Inferring lift and drag in an E-M plot -- 5.6 Aerodynamic efficiency (L/D) and performance efficiency (M(L/D)) -- 5.7 Dimensionalizing drag -- 5.8 Propulsive performance -- 5.9 Specific excess thrust and linear acceleration capability -- 5.10 Specific excess power, rate of climb (R.O.C.), and ceiling -- 5.11 Specific range -- 5.12 Loiter -- 5.13 Induced drag fraction of total drag for level flight limited by aerodynamics and propulsion -- 5.14 Maximum load factor, instantaneous turn rate and stall speed ratio -- 5.15 Combat agility, maximum sustained turn rate -- 327 $a6. Mission performance principles -- 6.1 Breguet range equation -- 6.2 Time-step integrating simulations -- 6.3 Creating missions using a mission simulation code -- 6.4 Observations examining the output of a mission simulation code -- 6.5 Creating trade studies using a mission simulation code -- 6.6 Creating payload/range charts using a mission simulation code -- Index. 330 3 $aThis book is a concise practical treatise for the student or experienced professional aircraft designer. This volume comprises key fundamental subjects for aerodynamic performance analysis: the basics of flight mechanics bridging both engineering and piloting perspectives, propulsion system performance attributes, practical drag prediction methods, aircraft "up and away" flight performance and aircraft mission performance. This book may serve as a textbook for an undergraduate aircraft performance course or as a reference for the classically trained practicing engineer. 410 0$aAerospace engineering collection. 606 $aAirplanes$xDesign and construction 606 $aAirplanes$xPerformance 615 0$aAirplanes$xDesign and construction. 615 0$aAirplanes$xPerformance. 676 $a629.1341 700 $aTakahashi$b Timothy$01493628 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910798269903321 996 $aAircraft performance and sizing$93716699 997 $aUNINA