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100   $a20151118d1973      ua             0
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181   $2rdacontent
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200 10$aComposite-overlay reinforcement of cutouts and cracks in metal sheet /$fRichard A. Mitchell; Ruth M. Woolley; Daniel J. Chwirut
210  1$aGaithersburg, MD :$cU.S. Dept. of Commerce, National Institute of Standards and Technology,$d1973.
215   $a1 online resource
225 1 $aNBSIR ;$v73-201
300   $a1973.
300   $aContributed record: Metadata reviewed, not verified. Some fields updated by batch processes.
300   $aTitle from PDF title page.
320   $aIncludes bibliographical references.
700   $aMitchell$b Richard A$026455
701   $aChwirut$b Daniel J$01390278
701   $aMitchell$b Richard A$026455
701   $aWoolley$b Ruth M$01390279
712 02$aUnited States.$bNational Bureau of Standards.
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912   $a9910710098803321
996   $aComposite-overlay reinforcement of cutouts and cracks in metal sheet$93442891
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100   $a20210805j194812    ua             0
101 0 $aeng
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181   $ctxt$2rdacontent
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200 14$aThe development of cambered airfoil sections having favorable lift characteristics at supercritical Mach numbers /$fby Donald J. Graham
210  1$aWashington :$cNational Advisory Committee for Aeronautics,$dDecember 1948.
215   $a1 online resource (82 pages) $cillustrations
225 1 $aNational Advisory Committee for Aeronautics technical note ;$v1771
300   $a"December 1948."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 17)
606   $aAirfoils$2nasat
606   $aAircraft stability$2nasat
606   $aAircraft control$2nasat
606   $aAerofoils$2fast
606   $aCamber (Aerofoils)$2fast
606   $aLift (Aerodynamics)$2fast
615  7$aAirfoils.
615  7$aAircraft stability.
615  7$aAircraft control.
615  7$aAerofoils.
615  7$aCamber (Aerofoils)
615  7$aLift (Aerodynamics)
700   $aGraham$b Donald J.$01411134
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
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996   $aThe development of cambered airfoil sections having favorable lift characteristics at supercritical Mach numbers$93501552
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