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200 10$aProceedings $eFirst International Symposium on 3D Data Processing Visualization and Transmission /$fInternational Symposium on 3D Data Processing, Visualization, and Transmission, Institute of Electrical and Electronics Engineers
210  1$aLos Alamitos :$cIEEE,$d2002.
215   $a1 online resource
311   $a0769515214 
330   $aThis text contains information on computer graphics as presented at the 1st International Symposium on 3D Data Processing, Visualization and Transmission (3DPVT 2002).
517   $a3D Data Processing Visualization and Transmission, 2002. Proceedings. First International Symposium on
531   $a3D DATA PROCESSING VISUALIZATION & TRANSMISSION, 2002. PROCEEDINGS. FIRST INTERNATIONAL SYMPOSIUM ON
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200 10$aEffect of hinge-line bleed on heat transfer and pressure distribution over a wedge-flap combination at Mach 10.4 /$fby H. Harris Hamilton, and J. David Dearing
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dAugust 1968.
215   $a1 online resource (44 pages) $cillustrations
225 1 $aNASA technical note ;$vTN D-4686
300   $a"August 1968."
320   $aIncludes bibliographical references (pages 18-21).
606   $aBoundary layer control
606   $aFlaps (Airplanes)
606   $aWedges
606   $aAircraft separation
606   $aAircraft separation$2fast
606   $aBoundary layer control$2fast
606   $aFlaps (Airplanes)$2fast
606   $aWedges$2fast
615  0$aBoundary layer control.
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615  0$aAircraft separation.
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615  7$aBoundary layer control.
615  7$aFlaps (Airplanes)
615  7$aWedges.
700   $aHamilton$b H. Harris$01405571
702   $aDearing$b J. David
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center.
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