00989nam--2200361---450-99000213345020331620100209121728.0978-88-420-8678-9000213345USA01000213345(ALEPH)000213345USA0100021334520041103d2009----km-y0itay50------baitaITy|||||||001yyPerché laicoStefano RodotàRomaBariLaterza2009193 p.21 cm<<I>> RobinsonLetture2001<<I>> RobinsonLettureLaicitàBNCF322.1RODOTÀ,Stefano166939ITsalbcISBD990002133450203316322.1 ROD 1215338 L.M.322.100255769BKECOMARIA1020041103USA011034ANNAMARIA9020100209USA011217Perché laico224492UNISA00978nam0-22003131i-450 99000527585040332120220905120907.0000527585FED01000527585(Aleph)000527585FED0100052758519990530d1974----km-y0itay50------bagery-------001yyPietismus und moderne Welt, mit Beiträgen von O. Söhngen, M. SchmidtK. Deppermann...[et al]hrsg. von Kurt AlandWittenLuther1974204 p.24 cmArbeiten zur Geschichte des Pietismus12Aland,KurtDeppermann,K.Söhngen,OskarSchmidt,M.ITUNINARICAUNIMARCBK990005275850403321ST.REL. 20-C 12ST.REL. 773FLFBCFLFBCPIETISMUS und moderne Welt, mit Beiträgen von O. Söhngen, M. Schmidt538770UNINA01808oam 2200493I 450 991071407720332120201105145052.0(CKB)5470000002506898(OCoLC)761182042(EXLCZ)99547000000250689820111115j196811 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierA method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /by Charlie M. Jackson, Jr., Wallace C. Sawyer, and Rudeen S. SmithWashington, D.C. :National Aeronautics and Space Administration,November 1968.1 online resource (102 pages) illustrationsNASA technical note ;NASA TN D-4865"November 1968."Includes bibliographical references (page 52).Aerodynamic loadNoses (Space vehicles)TestingAngle of attack (Aerodynamics)Aerodynamics, SupersonicTestingAerodynamic load.Noses (Space vehicles)Testing.Angle of attack (Aerodynamics)Aerodynamics, SupersonicTesting.Jackson Charlie M.1395048Sawyer Wallace C.Smith Rudeen S.United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCOOCLCQGPOBOOK9910714077203321A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow3519899UNINA