BL_Theory_Cf and Ch results_incomp&comp.pdf

BL_Theory_Cf and Ch results_incomp&comp.pdf - Six/1N...

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Unformatted text preview: Six/1N Fé‘licwo 0.010 C‘ J r' f= U a $0 °° ‘ Incomrrcsnbk 0,003.- 91.... 0.032 Fig. 7.10. Localcoefficient 0W? __ of skin friction on a. flat ' plate at zero incidence in incompressible flow, cleter- M005- mmed from direct. measure- [Mike-cf sh}: mm? measurement ment of shearing stress by 0.0m A 170'” WWW profile Liepmann and Dhawan 00002 Dried Ski}? Rib/rim measorammf, x ~28.6‘cm {6, 13] a I I I 1 I 1 x -56'Cffl Theory: laminar from eqn. (7.32); t b I tr . . H _l_ .l_| 111' u en rum eqn (211_2) (MW? ! i L LI_ 1 70‘ 2 .3 553105 2 3+,” ' x refer— “‘II I-II-I "I. is a ‘b h ---I WIIIII I‘ll—II r i I 2 - II-II b . a} H i I'll-"fl" la]! {iii Ii“ "U. ml- lllli. "' I a N I {i I! .lfl L. E m tun-III- IIII-IIIII IIIIII s I I I - [Ill-II-l-l (gs Q "I. Will Willie! f .5" IIIIIIV l s I - - - Fig. 23.6. Coefficient of total skin friction for an adiabatic flat. plate at zero incidence for laminar .nd turbulent boundary layer. Theoretical curves for turbulent flow from eqn. (23.31), after 3. R. van Driest [27]; y = 14, w = 0-76, F = 1 - ‘ HEAT TFPHQSFE’P- Laminar 5 _L. J— l__|_ _l l_ 10‘ 5 103 5 [0" 5 ‘107 5 108 ReJr FIGURE 6.30 Station number as a function of Reynolds and Mach numbers for an insulated flat plate. (From Van Driexr, Ref. 92.) ' In (MPH $5 {lair Mal Cmpmuilole L4H». Anoleuw) IH can-.(fl-sn'lale amt/l CWfJflJ)I“'-'I}‘¢ ...
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