Publication Date:
2019-07-13
Description:
An experimental study investigated the interactive effect between the heat transfer and the steady transonic flow in a simple convergent-divergent duct. The results show that the position of the shock is considerably affected by the effect of wall cooling. The physical explanation for the shift is also offered. The results may have implications in the other internal flow problems.
Keywords:
FLUID MECHANICS AND HEAT TRANSFER
Type:
AIAA PAPER 81-0275
,
Aerospace Sciences Meeting; Jan 12, 1981 - Jan 15, 1981; St. Louis, MO
Format:
text
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