02113cam a2200469Ia 4500011429535MiAaHDL20141009010000.0m d cr bn ---auaua060505s1969 dcua bt f000 0 eng dsdr-uiuc6382520(OCoLC)68225887FERFERLHLUIUUNAS 1.26:1332N69-3474469N34744RASA-68-10NASA CR 1332Crimi, Peter.A method for analyzing the aeroelastic stability of a helicopter rotor in forward flight /by Peter Crimi.Washington, D.C. :National Aeronautics and Space Administration ;Springfield, Va. :For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor],1969.iii, 107 p. :ill. ;27 cm.NASA contractor report ;NASA CR-1332"NASA CR-1332.""August 1969"--Cover.Includes bibliographical references (p. 106-107).Aerodynamic stability of helicopter rotor in forward flight.Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 11/15/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19690025366%5F1969025366.pdf.Prepared by Rochester Applied Science Associates, Inc., Rochester, N.Y. for Langley Research CenterNAS 1-7411Mode of access: Internet.Computer programs.Rotors (Helicopters)Aerodynamics.Rotors (Helicopters)Equations of motion.nasatDigital computers.nasatAerodynamic characteristics.nasatRotary wings.nasatHorizontal flight.nasatHelicopters.nasatAerodynamic stability.nasatApplied Science Associates.Langley Research Center.01142953520101025082155.020141009010000.020141112164151.02025-01-01T19:19:02Z2025-01-01T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6382520uiugSDRUIUCuiug.30112106581744UIUno.13326382520UIUUIUC20250101googleuiug.30112106581744no.13321969pdbibUS fed doc