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<![CDATA[PKK Library Search for 'su:{Pressure distribution}']]> /cgi-bin/koha/opac-search.pl?q=ccl=su%3A%7BPressure%20distribution%7D&format=rss2 4 0 200 NASA Technical Note: INCOMPRESSIBLY LUBRICATED RAYLEIGH STEP JOURNAL BEARING ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=393277 By Hamrock, Bernard J.. Washington, D.C. NASA 1968 . 30p. , Technical Note D-4831-4840 | Bound Vol. No.101114 contents TR7567-7575

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]]> /cgi-bin/koha/opac-detail.pl?biblionumber=393277 Pressure distribution over an N.A.C.A.23012 airfoil with a slotted and a plan flap ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=564089 By Wenzinger,Carl J.. Washington,D.C. National Advisory Committee For Aeronautics 1938 . 32p.

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]]> /cgi-bin/koha/opac-detail.pl?biblionumber=564089 Effects of boundary layer displacement and leading edge bluntness on pressure distribution, skin friction, and heat transfer of bodies at hypersonic speeds [NACA TN-4301] ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=564267 By Bertram, Mitchel H.. Washington, D. C. National Aeronautics and Space Administration 1958 . 25p

Place Hold on Effects of boundary layer displacement and leading edge bluntness on pressure distribution, skin friction, and heat transfer of bodies at hypersonic speeds [NACA TN-4301]

]]> /cgi-bin/koha/opac-detail.pl?biblionumber=564267 NASA Technical Note :Flight pressure distributions on the vertical stablizers and speed brakes of the X-15 airplane at mach numbers from 1 to 6 ISBN /cgi-bin/koha/opac-detail.pl?biblionumber=565976 Washington, D.C. NASA 1965 . 54p. , Technical Note D-3041-3050

Place Hold on NASA Technical Note :Flight pressure distributions on the vertical stablizers and speed brakes of the X-15 airplane at mach numbers from 1 to 6

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