00695oam 2200241z- 450 991052488010332120170925193918.00-8142-7154-5(CKB)3780000000104869(EXLCZ)99378000000010486920161211c2009uuuu -u- -engAmerican husband /Kary WaysonThe Ohio State University PressA volume of poetry about motherhood, travel, being.American poetry21st centuryAmerican poetry811/.6Wayson Kary1970-1237696BOOK9910524880103321American husband2872990UNINA02777oam 2200685 450 991070747330332120240208235201.0(CKB)5470000002464793(OCoLC)785231998(EXLCZ)99547000000246479320120408j198009 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 /Kevin W. Noonan and Gene J. Bingham[Washington, D.C.] :National Aeronautics and Space Administration, Scientific and Technical Information Branch,September 1980.1 online resource (82 pages) chiefly illustrationsNASA technical paper ;1701AVRADCOM technical report ;80-B-5Title from title screen (viewed on Aug. 16, 2016)."September 1980.""Performing Organization: NASA Langley Research Center and Structures Laboratory, AVRADCOM Research and Technology Laboratories"--Report documentation page.Includes bibliographical references (page 13).Aerodynamic characteristicsnasatAirfoilsnasatHelicoptersnasatReynolds numbernasatWind tunnel testsnasatAerofoilsTestingfastHelicoptersAerodynamicsfastReynolds numberfastRotors (Helicopters)TestingfastAerodynamic characteristics.Airfoils.Helicopters.Reynolds number.Wind tunnel tests.AerofoilsTesting.HelicoptersAerodynamics.Reynolds number.Rotors (Helicopters)Testing.Noonan Kevin W.1396266Bingham Gene J.Langley Research Center.United States.Army Aviation Research and Development Command.Army Research and Technology Laboratories (U.S.).Structures Laboratory.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,OCLCEOCLCEOCLCQOCLCOOCLCFOCLCQGPOBOOK9910707473303321Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.903456069UNINA