01551cam2 22003131 450 SOBE0004290820140507115955.020140506g00009999|||||ita|0103 bagerDE<<129: >>Philosophia methodo scientiis propria explanataBenedikt StattlerHildesheimZürichNew YorkOlms Verlag8 v.21 cm001SOBE000180942001 <<3. Abteilung: >>Materialien und Dokumente [101- ]001SOBE000429092000 <<Pars1 : >>Logica / Benedikt Stattler ; mit einem Vorwort von Karlheinz Ruhstorfer001SOBE000429182000 <<Pars 2 : >>Ontologia / Benedikt Stattler001SOBE000429242000 <<Pars 3 : >>Cosmologia / Benedikt Stattler001SOBE000429432000 <<Pars 4 : >>Psychologia / Benedikt Stattler001SOBE000429442000 <<Pars 5 : >>Theologia naturalis / Benedikt Stattler001SOBE000429452000 <<Pars 6: >>Physica generalis / Benedikt Stattler001SOBE000429462000 <<Pars 7: >>Physica particularis corporum titalium huius mundi / Benedikt Stattler001SOBE000429482000 <<Pars 8: >>Physica particularis corporum partialium telluris nostrae / Benedikt StattlerStattler, BenediktA600200062265070163841ITUNISOB20140507RICASOBE00042908M 102 Monografia moderna SBNMPhilosophia methodo scientiis propria explanata1710972UNISOB01505oam 2200445 450 991071701200332120220218115047.0(CKB)5470000002528090(OCoLC)1291212594(OCoLC)995470000002528090(EXLCZ)99547000000252809020220106j199204 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierAeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model /Aparajit J. Mahajan [and three others]Washington, D.C. :NASA,April 1992.1 online resource (approximately 14 pages) illustrationsNASA/TM ;105268"April 1992."Includes bibliographical references (pages 6-7).Prop-fan technologynasatFlutternasatCruise missilesnasatProp-fan technology.Flutter.Cruise missiles.Mahajan Aparajit J(Aparajit Jagannath),1419987United States.National Aeronautics and Space Administration,GPOGPOGPOOCLCOGPOBOOK9910717012003321Aeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model3536332UNINA