01246nam2-2200385li-450 99000017994020331620180312154903.0981-02-1309-30017994USA010017994(ALEPH)000017994USA0100179942001995011994-------y0itay0103----baengSGUnder the spell of the Gauge principleG.'t HooftSingapore [etc.]World Scientificcopyr. 1994XI, 683 p.ill.24 cmAdvanced series in mathematical physics1900100179912001Advanced series in mathematical physicsTeoria di gauge530.143 5Teoria di GaugeHOOFT,G.'t464413Sistema bibliotecario di Ateneo dell' Università di SalernoRICA990000179940203316530.143 5 HOO0016448/CBS530.143 500325525BKSCI1995013120001110USA01171320020403USA011625PATRY9020040406USA011613RSIAV79020090731USA010933Under the spell of the Gauge principle192644UNISA01937oam 2200517 450 991070743970332120160825110957.0(CKB)5470000002465132(OCoLC)760918532(EXLCZ)99547000000246513220111114j198012 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierLeading-edge deflection optimization for a highly swept arrow-wing configuration /Paul L. Coe, Jr., Jarrett K. Huffman, and James W. Fenbert[Washington, D.C.] :National Aeronautics and Space Administration, Scientific and Technical Information Branch,December 1980.1 online resource (56 pages) illustrationsNASA technical paper ;1777Title from title screen (viewed on Aug. 25, 2016)."December 1980.""Performing Organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 55-56).AerodynamicsfastAirplanesWings, Swept-backfastLeading edges (Aerodynamics)fastAerodynamics.AirplanesWings, Swept-back.Leading edges (Aerodynamics)Coe Paul L.1401937Huffman Jarrett K.Fenbert James W.Langley Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,OCLCEOCLCEOCLCQOCLCFOCLCQOCLCOGPOBOOK9910707439703321Leading-edge deflection optimization for a highly swept arrow-wing configuration3471390UNINA