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101 0 $aeng
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181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLocal skin friction coefficients and boundary-layer profiles obtained in flight from the XB-70-1 airplane at Mach numbers up to 2.5 /$fby David F. Fisher and Edwin J. Saltzman
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dJune 1973.
215   $a1 online resource (68 pages) $cillustrations
225 1 $aNASA/TN ;$vD-7220
300   $a"June 1973."
320   $aIncludes bibliographical references (pages 14-15).
606   $aTurbulent boundary layer$2nasat
606   $aSkin friction$2nasat
606   $aFluid mechanics$2nasat
606   $aSkin friction (Aerodynamics)
606   $aB-70 bomber
606   $aB-70 bomber$2fast
606   $aSkin friction (Aerodynamics)$2fast
606   $aTurbulent boundary layer$2fast
615  7$aTurbulent boundary layer.
615  7$aSkin friction.
615  7$aFluid mechanics.
615  0$aSkin friction (Aerodynamics)
615  0$aB-70 bomber.
615  7$aB-70 bomber.
615  7$aSkin friction (Aerodynamics)
615  7$aTurbulent boundary layer.
700   $aFisher$b David F.$059946
702   $aSaltzman$b Edwin J.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aFlight Research Center (U.S.)
801  0$bABC
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801  2$bOCLCQ
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906   $aBOOK
912   $a9910716676203321
996   $aLocal skin friction coefficients and boundary-layer profiles obtained in flight from the XB-70-1 airplane at Mach numbers up to 2.5$93537952
997   $aUNINA