Abstract:561g Q '(t, oo) = (l/u e ) dwjdt ; 0 2 '({, (») = 0 0 0 K.°o)=l; 02(£oo) = 0 3 « f oo) = 0 and at the wall, /o'«. 0) =/ 2 '«, 0) =/,'«, 0) = 0 0o'«.0) = 0; 0 2 '(£,0)=1 0&.0) = TJT e ; 0 2 (£,0) = 0 3 (£,0) = 0
ExampleAs a numerical example Eqs. (4) and (6) were solved for a spinning 11-cm-diam tangent-ogive cylinder at a Mach number of 3.0 and at 4.0° incidence 5 by the techniques described in Ref. 6. Typical results for one axial body station are summarized in Figs. 1 and 2. The results indicate that there i… Show more
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