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- W2006432731 abstract "symmetrically over the surface becomes highly nonuniform at increasing body and angle of attack, generating a region of lower temperature on the leeward side and a region of higher temperature on the windward side. In practical applications a lower average temperature and then a higher average heat transfer rate are inevitable for the entire surface to maintain every point below the maximum permissible temperature for the material used. To minimize the severe deterioration of the cooling capability of slot injection due to three-dimensional effects, new designs are required for the slot system which give a nonuniform peripheral distribution of the coolant. At this purpose a very simple slot system scheme which counters the cross-flow effects has been investigated in the present study. The scheme consists of nonsymmetric slots, higher on the windward side and lower on the leeward side which, maintaining the average height Seq = (SL + Sw)/2, i.e., the injection coolant mass flow, and producing a nonuniform injection pattern, act to prevent and reduce the negative cross-flow effects on cooling. The experimental results (Fig. 5), compared with the previous symmetric slot results, generate a more uniform adiabatic wall temperature distribution and thus improve the cooling capability of the system. The results obtained with this primitive nonsymmetric slot scheme are only indicative, however they can suggest a possible direction of investigation." @default.
- W2006432731 created "2016-06-24" @default.
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- W2006432731 date "1975-07-01" @default.
- W2006432731 modified "2023-09-27" @default.
- W2006432731 title "Analysis of Predicted Aircraft Wake Vortex Transport and Comparison with Experiment" @default.
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- W2006432731 doi "https://doi.org/10.2514/3.59843" @default.
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