LEADER 03697nam 22007092 450 001 9910789315103321 005 20151005020622.0 010 $a1-107-23693-2 010 $a1-107-34191-4 010 $a1-107-34441-7 010 $a1-107-25562-7 010 $a1-139-23565-6 010 $a1-107-34816-1 010 $a1-107-34566-9 035 $a(CKB)3460000000128984 035 $a(EBL)1139714 035 $a(OCoLC)841927259 035 $a(SSID)ssj0000872160 035 $a(PQKBManifestationID)11471602 035 $a(PQKBTitleCode)TC0000872160 035 $a(PQKBWorkID)10824632 035 $a(PQKB)11065935 035 $a(UkCbUP)CR9781139235655 035 $a(MiAaPQ)EBC1139714 035 $a(Au-PeEL)EBL1139714 035 $a(CaPaEBR)ebr10695284 035 $a(CaONFJC)MIL485873 035 $z(PPN)261295942 035 $a(PPN)190626372 035 $a(EXLCZ)993460000000128984 100 $a20120123d2013|||| uy| 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aRotorcraft aeromechanics /$fWayne Johnson, NASA Ames Research Center$b[electronic resource] 210 1$aCambridge :$cCambridge University Press,$d2013. 215 $a1 online resource (xix, 927 pages) $cdigital, PDF file(s) 225 1 $aCambridge aerospace series ;$v36 300 $aTitle from publisher's bibliographic system (viewed on 05 Oct 2015). 311 $a1-107-02807-8 311 $a1-107-35778-0 320 $aIncludes bibliographical references and index. 327 $aMachine generated contents note: 1. Introduction; 2. Notation; 3. Hover; 4. Vertical flight; 5. Forward flight wake; 6. Forward flight; 7. Performance; 8. Design; 9. Wings and wakes; 10. Unsteady aerodynamics; 11. Actuator disk; 12. Stall; 13. Computational aerodynamics; 14. Noise; 15. Mathematics of rotating systems; 16. Blade motion; 17. Beam theory; 18. Dynamics; 19. Flap motion; 20. Stability; 21. Flight dynamics; 22. Comprehensive analysis. 330 $aA rotorcraft is a class of aircraft that uses large-diameter rotating wings to accomplish efficient vertical take-off and landing. The class encompasses helicopters of numerous configurations (single main rotor and tail rotor, tandem rotors, coaxial rotors), tilting proprotor aircraft, compound helicopters, and many other innovative configuration concepts. Aeromechanics covers much of what the rotorcraft engineer needs: performance, loads, vibration, stability, flight dynamics, and noise. These topics include many of the key performance attributes and the often-encountered problems in rotorcraft designs. This comprehensive book presents, in depth, what engineers need to know about modelling rotorcraft aeromechanics. The focus is on analysis, and calculated results are presented to illustrate analysis characteristics and rotor behaviour. The first third of the book is an introduction to rotorcraft aerodynamics, blade motion, and performance. The remainder of the book covers advanced topics in rotary wing aerodynamics and dynamics. 410 0$aCambridge aerospace series ;$v36. 606 $aHelicopters$xAerodynamics 606 $aHelicopters$xDesign and construction 606 $aRotors (Helicopters) 615 0$aHelicopters$xAerodynamics. 615 0$aHelicopters$xDesign and construction. 615 0$aRotors (Helicopters) 676 $a629.132/3 686 $aTEC009000$2bisacsh 700 $aJohnson$b Wayne$f1946-$0770555 801 0$bUkCbUP 801 1$bUkCbUP 906 $aBOOK 912 $a9910789315103321 996 $aRotorcraft aeromechanics$93747656 997 $aUNINA