02200cam a2200469Ia 4500011429414MiAaHDL20141009010000.0m d cr bn ---auaua060517s1971 dcu t f000 0 eng d19720006328N721397772N13977sdr-uiuc6381305(OCoLC)68934883FERFERFEREGMUIUUSadler, S. G.Development and application of a method for predicting rotor free wake positions and resulting rotor blade air loads.Volume 2,Program listings /by S. Gene Sadler.Washington, D.C. :National Aeronautics and Space Administration ;Springfield, Va. :For sale by the National Technical Information Service [distributor],1971.147 p. ;27 cm.NASA contractor report ;NASA CR-1912"NASA CR-1912.""December 1971."Cover title.Computer program listings are presented for two separate programs: the wake geometry 1 blade loads and response. These listings correspond to the calculations discussed previously.Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 04/05/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19720006328%5f1972006328.pdf.Performed by Rochester Applied Science Associates, Inc., Rochester, N.Y., for Langley Research CenterNAS1-8448Mode of access: Internet.Input/output routines.nasatWakes.nasatRotor blades (turbomachinery).nasatDynamic response.nasatComputer programs.nasatAerodynamic loads.nasatInput-output analysis.Wakes (Aerodynamics)Blades.Rotors.Frequency response (Dynamics)Aerodynamic load.Langley Research Center.Rochester Applied Sciences Associates.01142941420101022143512.020141009010000.020141112164151.02024-04-22T18:14:21ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6381305uiugSDRUIUCuiug.30112106856930UIU6381305UIUUIUC20240422googleuiug.301121068569301971pdbibUS fed doc--NTIS: pubdate < 2020