LEADER 01886nam 2200577 450 001 996466488603316 005 20220818172751.0 010 $a3-540-37034-X 024 7 $a10.1007/BFb0070208 035 $a(CKB)1000000000438185 035 $a(SSID)ssj0000321563 035 $a(PQKBManifestationID)12116347 035 $a(PQKBTitleCode)TC0000321563 035 $a(PQKBWorkID)10264673 035 $a(PQKB)11155822 035 $a(DE-He213)978-3-540-37034-5 035 $a(MiAaPQ)EBC5595748 035 $a(Au-PeEL)EBL5595748 035 $a(OCoLC)1076264505 035 $a(MiAaPQ)EBC6812174 035 $a(Au-PeEL)EBL6812174 035 $a(OCoLC)793078438 035 $a(PPN)155193635 035 $a(EXLCZ)991000000000438185 100 $a20220818d1977 uy 0 101 0 $aeng 135 $aurnn|008mamaa 181 $ctxt 182 $cc 183 $acr 200 14$aThe axiom of constructibility $ea guide for the mathematician /$fKeith J. Devlin 205 $a1st ed. 1977. 210 1$aHeidelberg ;$aBerlin ;$aNew York :$cSpringer-Verlag,$d[1977] 210 4$dİ1977 215 $a1 online resource (X, 98 p.) 225 1 $aLecture notes in mathematics (Springer-Verlag) ;$v617 300 $aBibliographic Level Mode of Issuance: Monograph 311 $a3-540-08520-3 327 $aFour famous problems -- What is set theory? -- The axiom of constructibility -- Applications of V=L in mathematics -- A problem in measure theory. 410 0$aLecture notes in mathematics (Springer-Verlag) ;$v617. 606 $aAxiom of constructibility 615 0$aAxiom of constructibility. 676 $a511.322 700 $aDevlin$b Keith J.$028052 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a996466488603316 996 $aThe axiom of constructibility$92906397 997 $aUNISA LEADER 02947oam 2200709 450 001 9910716544203321 005 20210625153908.0 035 $a(CKB)5470000002522714 035 $a(OCoLC)24267960$z(OCoLC)762065336 035 $a(OCoLC)995470000002522714 035 $a(EXLCZ)995470000002522714 100 $a19910821j197312 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 14$aThe effects of an autopilot on airplane responses to turbulence with emphasis on tail loads /$fby Boyd Perry III 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dDecember 1973. 215 $a1 online resource (i, 51 pages) $cillustrations 225 1 $aNASA/TN ;$vD-7231 300 $a"December 1973." 320 $aIncludes bibliographical references (page 28). 330 $aAn analytical study has been made to assess the loads developed on the horizontal tail of an autopilot-controlled rigid airplane flying in one-dimensional atmospheric turbulence. The root-mean-square values of rigid-airframe responses and tail-load responses were calculated at five flight conditions, and the behavior of these responses was observed in two autopilot modes: pitch-attitude-hold mode and altitude-control mode. It was found that pitch attitude and altitude can be controlled by the simple autopilot with acceptable or no increases in tail loads. 606 $aAerodynamic loads$2nasat 606 $aAtmospheric turbulence$2nasat 606 $aAutomatic pilot (Airplanes) 606 $aAirplanes$xHandling characteristics 606 $aAirplanes$xTail surfaces 606 $aAerodynamic load 606 $aAerodynamic load$2fast 606 $aAirplanes$xHandling characteristics$2fast 606 $aAirplanes$xTail surfaces$2fast 606 $aAtmospheric turbulence$2fast 606 $aAutomatic pilot (Airplanes)$2fast 615 7$aAerodynamic loads. 615 7$aAtmospheric turbulence. 615 0$aAutomatic pilot (Airplanes) 615 0$aAirplanes$xHandling characteristics. 615 0$aAirplanes$xTail surfaces. 615 0$aAerodynamic load. 615 7$aAerodynamic load. 615 7$aAirplanes$xHandling characteristics. 615 7$aAirplanes$xTail surfaces. 615 7$aAtmospheric turbulence. 615 7$aAutomatic pilot (Airplanes) 700 $aPerry$b Boyd$01389770 712 02$aUnited States.$bNational Aeronautics and Space Administration, 712 02$aLangley Research Center. 801 0$bABC 801 1$bABC 801 2$bAD# 801 2$bOCLCE 801 2$bOCLCQ 801 2$bOCLCO 801 2$bOCLCF 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910716544203321 996 $aThe effects of an autopilot on airplane responses to turbulence with emphasis on tail loads$93510622 997 $aUNINA