LEADER 01241aam 2200373I 450 001 9910710267703321 005 20160121100810.0 024 8 $aGOVPUB-C13-89cac9b63622a9d4def34542b4ae0eee 035 $a(CKB)5470000002476608 035 $a(OCoLC)935500315 035 $a(EXLCZ)995470000002476608 100 $a20160121d1981 ua 0 101 0 $aeng 181 $2rdacontent 182 $2rdamedia 183 $2rdacarrier 200 12$aA discussion of gridnet simulation results /$fR. T. Moore 210 1$aGaithersburg, MD :$cU.S. Dept. of Commerce, National Institute of Standards and Technology,$d1981. 215 $a1 online resource 225 1 $aNBSIR ;$v81-2414 300 $a1981. 300 $aContributed record: Metadata reviewed, not verified. Some fields updated by batch processes. 300 $aTitle from PDF title page. 320 $aIncludes bibliographical references. 700 $aMoore$b Raymond T$0270845 701 $aMoore$b Raymond T$0270845 712 02$aUnited States.$bNational Bureau of Standards. 801 0$bNBS 801 1$bNBS 801 2$bGPO 906 $aBOOK 912 $a9910710267703321 996 $aA discussion of gridnet simulation results$93452877 997 $aUNINA LEADER 01987oam 2200565 450 001 9910717128003321 005 20220210124522.0 035 $a(CKB)5470000002528938 035 $a(OCoLC)1156324021 035 $a(EXLCZ)995470000002528938 100 $a20200602d1940 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aWind-tunnel investigation of an N.A.C.A. 23030 airfoil with various arrangements of slotted flaps /$fby I.G. Recant 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1940. 215 $a1 online resource (13 pages, 19 unnumbered pages) $cillustrations 225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vno. 755 300 $a"March 1940." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 12). 606 $aAirplanes$xWings 606 $aFlaps (Airplanes) 606 $aSlotted flaps (Airplanes) 606 $aWind tunnel testing 606 $aAirplanes$xWings$2fast 606 $aFlaps (Airplanes)$2fast 606 $aSlotted flaps (Airplanes)$2fast 606 $aWind tunnel testing$2fast 615 0$aAirplanes$xWings. 615 0$aFlaps (Airplanes) 615 0$aSlotted flaps (Airplanes) 615 0$aWind tunnel testing. 615 7$aAirplanes$xWings. 615 7$aFlaps (Airplanes) 615 7$aSlotted flaps (Airplanes) 615 7$aWind tunnel testing. 700 $aRecant$b Isidore G.$01386872 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bTRAAL 801 1$bTRAAL 801 2$bOCLCO 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910717128003321 996 $aWind-tunnel investigation of an N.A.C.A. 23030 airfoil with various arrangements of slotted flaps$93524930 997 $aUNINA LEADER 04404nam 22008295 450 001 9910254610503321 005 20200706094548.0 010 $a4-431-55882-9 024 7 $a10.1007/978-4-431-55882-8 035 $a(CKB)3710000000526964 035 $a(EBL)4182844 035 $a(SSID)ssj0001597193 035 $a(PQKBManifestationID)16297865 035 $a(PQKBTitleCode)TC0001597193 035 $a(PQKBWorkID)14885895 035 $a(PQKB)11755498 035 $a(DE-He213)978-4-431-55882-8 035 $a(MiAaPQ)EBC4182844 035 $a(PPN)190886749 035 $a(EXLCZ)993710000000526964 100 $a20151201d2016 u| 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aClassical Pendulum Feels Quantum Back-Action /$fby Nobuyuki Matsumoto 205 $a1st ed. 2016. 210 1$aTokyo :$cSpringer Japan :$cImprint: Springer,$d2016. 215 $a1 online resource (110 p.) 225 1 $aSpringer Theses, Recognizing Outstanding Ph.D. Research,$x2190-5053 300 $a"Doctoral Thesis accepted by the University of Tokyo, Tokyo, Japan." 311 $a4-431-55880-2 320 $aIncludes bibliographical references at the end of each chapters. 327 $aIntroduction -- Theory of Optomechanics -- Application of Optomechanics -- Optical Torsional Spring -- Experimental Setup -- Experimental Results -- The Future -- Conclusions. . 330 $aIn this thesis, ultimate sensitive measurement for weak force imposed on a suspended mirror is performed with the help of a laser and an optical cavity for the development of gravitational-wave detectors. According to the Heisenberg uncertainty principle, such measurements are subject to a fundamental noise called quantum noise, which arises from the quantum nature of a probe (light) and a measured object (mirror). One of the sources of quantum noise is the quantum back-action, which arises from the vacuum fluctuation of the light. It sways the mirror via the momentum transferred to the mirror upon its reflection for the measurement. The author discusses a fundamental trade-off between sensitivity and stability in the macroscopic system, and suggests using a triangular cavity that can avoid this trade-off. The development of an optical triangular cavity is described and its characterization of the optomechanical effect in the triangular cavity is demonstrated. As a result, for the first time in the world the quantum back-action imposed on the 5-mg suspended mirror is significantly evaluated. This work contributes to overcoming the standard quantum limit in the future. 410 0$aSpringer Theses, Recognizing Outstanding Ph.D. Research,$x2190-5053 606 $aQuantum theory 606 $aLasers 606 $aPhotonics 606 $aAstronomy$vObservations 606 $aAstronomy?Observations 606 $aAstrophysics 606 $aLow temperatures 606 $aLow temperatures 606 $aQuantum Physics$3https://scigraph.springernature.com/ontologies/product-market-codes/P19080 606 $aOptics, Lasers, Photonics, Optical Devices$3https://scigraph.springernature.com/ontologies/product-market-codes/P31030 606 $aAstronomy, Observations and Techniques$3https://scigraph.springernature.com/ontologies/product-market-codes/P22014 606 $aAstrophysics and Astroparticles$3https://scigraph.springernature.com/ontologies/product-market-codes/P22022 606 $aLow Temperature Physics$3https://scigraph.springernature.com/ontologies/product-market-codes/P25130 615 0$aQuantum theory. 615 0$aLasers. 615 0$aPhotonics. 615 0$aAstronomy 615 0$aAstronomy?Observations. 615 0$aAstrophysics. 615 0$aLow temperatures. 615 0$aLow temperatures. 615 14$aQuantum Physics. 615 24$aOptics, Lasers, Photonics, Optical Devices. 615 24$aAstronomy, Observations and Techniques. 615 24$aAstrophysics and Astroparticles. 615 24$aLow Temperature Physics. 676 $a531.324 700 $aMatsumoto$b Nobuyuki$4aut$4http://id.loc.gov/vocabulary/relators/aut$0815563 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910254610503321 996 $aClassical Pendulum Feels Quantum Back-Action$91820608 997 $aUNINA