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181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic 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 /$fKevin W. Noonan and Gene J. Bingham
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dSeptember 1980.
215   $a1 online resource (82 pages) $cchiefly illustrations
225 1 $aNASA technical paper ;$v1701
225 1 $aAVRADCOM technical report ;$v80-B-5
300   $aTitle from title screen (viewed on Aug. 16, 2016).
300   $a"September 1980."
300   $a"Performing Organization: NASA Langley Research Center and Structures Laboratory, AVRADCOM Research and Technology Laboratories"--Report documentation page.
320   $aIncludes bibliographical references (page 13).
606   $aAerodynamic characteristics$2nasat
606   $aAirfoils$2nasat
606   $aHelicopters$2nasat
606   $aReynolds number$2nasat
606   $aWind tunnel tests$2nasat
606   $aAerofoils$xTesting$2fast
606   $aHelicopters$xAerodynamics$2fast
606   $aReynolds number$2fast
606   $aRotors (Helicopters)$xTesting$2fast
615  7$aAerodynamic characteristics.
615  7$aAirfoils.
615  7$aHelicopters.
615  7$aReynolds number.
615  7$aWind tunnel tests.
615  7$aAerofoils$xTesting.
615  7$aHelicopters$xAerodynamics.
615  7$aReynolds number.
615  7$aRotors (Helicopters)$xTesting.
700   $aNoonan$b Kevin W.$01396266
702   $aBingham$b Gene J.
712 02$aLangley Research Center.
712 02$aUnited States.$bArmy Aviation Research and Development Command.
712 02$aArmy Research and Technology Laboratories (U.S.).$bStructures Laboratory.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
801  0$bOCLCE
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801  2$bOCLCQ
801  2$bOCLCO
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801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707473303321
996   $aAerodynamic 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$93456069
997   $aUNINA