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美国政府科技报告
>BOUNDARY-LAYER SIMILAR SOLUTIONS AND CORRELATION EQUATIONS FOR LAMINAR HEAT-TRANSFER DISTRIBUTION IN EQUILIBRIUMnAIR AT VELOCITIES UP TO 41,100 FEET PER SECOND
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BOUNDARY-LAYER SIMILAR SOLUTIONS AND CORRELATION EQUATIONS FOR LAMINAR HEAT-TRANSFER DISTRIBUTION IN EQUILIBRIUMnAIR AT VELOCITIES UP TO 41,100 FEET PER SECOND
Locally similar solutions of the laminar boundary-layer equations are obtained for air at chemical equilibrium for static enthalpies up to l,000RTref (corresponding to the free-stream stagnation enthalpy for atmospheric flight at velocities up to 4.1,100 feet per second). Correlation of the transport property estimates of NASA TR R-50 are employed in the solutions.nExact solutions for flat-plate flow, axisymmetric stagnation flow, and stagnation flow for a yawed infinite cylinder are obtained and correlating formulas for the appropriate heat-transfer functions are devel¬oped
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