LEADER 03713nam 2200625 a 450 001 9910824305403321 005 20230725052313.0 010 $a1-60086-752-9 010 $a1-61344-046-4 035 $a(CKB)3390000000018386 035 $a(EBL)3111641 035 $a(OCoLC)922978856 035 $a(SSID)ssj0000550785 035 $a(PQKBManifestationID)12207215 035 $a(PQKBTitleCode)TC0000550785 035 $a(PQKBWorkID)10509282 035 $a(PQKB)11231989 035 $a(Au-PeEL)EBL3111641 035 $a(CaPaEBR)ebr10516746 035 $a(MiAaPQ)EBC3111641 035 $a(EXLCZ)993390000000018386 100 $a20100420d2010 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aFundamentals of aircraft and airship design$hVolume 1$iAircraft design$b[electronic resource] /$fLeland M. Nicolai, Grant E. Carichner 210 $aReston, Va. $cAmerican Institute of Aeronautics and Astronautics$d2010 215 $a1 online resource (931 p.) 225 1 $aAIAA educational series 300 $aRev. and expanded ed. of: Fundamentals of aircraft design / Leland M. Nicolai. 1975. 311 $a1-60086-751-0 320 $aIncludes bibliographical references and index. 327 $aCOVER; TITLE; COPYRIGHT; FOREWORD; CONTENTS; LIST OF COLOR PLATES; PREFACE; Chapter 1: Introduction; Chapter 2: Review of Practical Aerodynamics; Chapter 3: Aircraft Performance Methods; Chapter 4: Aircraft Operating Envelope; Chapter 5: Preliminary Estimate of Takeoff Weight; Chapter 6: Estimating theTakeoff Wing Loading; Chapter 7: Selecting the Planform and Airfoil Section; Chapter 8: Preliminary Fuselage Sizing and Design; Chapter 9: High-Lift Devices; Chapter 10: Takeoff and Landing Analysis; Chapter 11: Preliminary Sizing of the Vertical and Horizontal Tails 327 $aChapter 12: Designing for Survivability (Stealth)Chapter 13: Estimating Wing-Body Aerodynamics; Chapter 14: Propulsion System Fundamentals; Chapter 15: Turbine Engine Inlet Design; Chapter 16: Corrections forTurbine Engine Installation; Chapter 17: Propeller Propulsion Systems; Chapter 18: Propulsion System Thrust Sizing; Chapter 19: Structures and Materials; Chapter 20: Refined Weight Estimate; Chapter 21 Static Stability and Control; Chapter 22: Trim Drag and Maneuvering Flight; Chapter 23: Control Surface Sizing Criteria; Chapter 24: Life Cycle Cost; Chapter 25: Trade Studies and Sizing 327 $aAppendix A: ConversionsAppendix B: Atmospheric Data; Appendix C: Isentropic Compressible Flow Functions; Appendix D: Normal Shock Functions for a Perfect Gas; Appendix E: Plane Oblique and Conical Shocks; Appendix F: NACA Airfoil Nomenclature and Data; Appendix G: Aerodynamic Data of Real Aircraft; Appendix H: Aerodynamics of Wing-Body Combinations; Appendix I: Aircraft Weights Data; Appendix J: Propulsion Data; Appendix K: Miscellaneous Data; INDEX; SUPPORTING MATERIALS 410 0$aAIAA educational series. 606 $aAirplanes$xDesign and construction$xHistory 606 $aAirships$xDesign and construction$xHistory 606 $aAeronautics$vPictorial works 615 0$aAirplanes$xDesign and construction$xHistory. 615 0$aAirships$xDesign and construction$xHistory. 615 0$aAeronautics 676 $a629.134/1 700 $aNicolai$b Leland M$g(Leland Malcolm)$0516655 701 $aCarichner$b Grant$0516656 701 $aNicolai$b Leland M$g(Leland Malcolm).$0516655 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910824305403321 996 $aFundamentals of aircraft and airship design$9845351 997 $aUNINA