01076nam--2200361---450-99000321700020331620090409134645.01436808774000321700USA01000321700(ALEPH)000321700USA0100032170020090409d--------km-y0itay50------baengUS||||||||001yyClotel, or, The president’s daughtera narrative of slave life in the United StatesWith a sketch of the author’s lifeWilliam Wells Brown[s.l.]Kessinger publishing[s.d.]VIII, 245 p.23 cm20012001001-------2001Letteratura americanaNarrativa810BROWN,William Wells603560ITsalbcISBD990003217000203316II.8.A.1969097 DSLLBKDSLLDSLL9020090409USA011346Clotel, or, The president’s daughter1011525UNISA01082nam a2200229 i 450099100139326970753620020507192645.0950607s1974 it ||| | ita b10841350-39ule_instLE01311608ExLDip.to MatematicaengMonteforte, Franco536997Su talune formule di quadratura generalizzata. Tesi di laurea /laureando Franco Monteforte ; relat. Maria Laura LeuzziLecce :Università degli studi. Facoltà di Scienze. Corso di laurea in Matematica,a.a. 1974-75Leuzzi, M. Laura.b1084135002-04-1428-06-02991001393269707536LE013 TES 1974/75 MON1 C.212013000029443le013-E0.00-l- 00000.i1095138628-06-02LE013 TES 1974/75 MON1 C.112013000030081le013-E0.00-l- 00000.i1095139828-06-02Su talune formule di quadratura generalizzata. Tesi di laurea918981UNISALENTOle01301-01-95ma -engxx 0202336nam 2200517 450 991070659080332120171114105131.0(CKB)5470000002456535(OCoLC)1011356298(EXLCZ)99547000000245653520171113j200102 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierSupersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system /J.R. DeBonis and C.J. TrefnyCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,February 2001.1 online resource (18 pages) illustrationsNASA/TM ;2001-210567"February 2001.""Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting sponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000.""Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.Includes bibliographical references (page 5).Supersonic wind tunnel tests of a half-axisymmetric 12 degree spike inlet to a rocket-based combined-cycle propulsion systemAir breathing boostersnasatHypersonic speednasatComputational fluid dynamicsnasatWind tunnel testsnasatPropulsionnasatPressure distributionnasatAir breathing boosters.Hypersonic speed.Computational fluid dynamics.Wind tunnel tests.Propulsion.Pressure distribution.DeBonis James R.1387413Trefny Charles J.NASA Glenn Research Center,GPOGPOBOOK9910706590803321Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system3444583UNINA