01505oam 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