The effect of periodic unsteady wakes on boundary layer transition and heat transfer on a curved plate /
all wake passing frequencies. Local Stanton numbers were
| Main Author: | |
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| Format: | Thesis eBook |
| Language: | English |
| Published: |
[Place of publication not identified] :
[publisher not identified] ;
1996.
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| Subjects: | |
| Online Access: | Link to OAKTrust copy |
| Summary: | all wake passing frequencies. Local Stanton numbers were also calculated on the concave surface and compared to analyzed using time-averaged and ensemble averaged boundary layer measurement were taken, and the data were boundary layer transition was investigated on a constant concave surface of the heat transfer plate to help explain curvature heat transfer curved plate in a subsonic wind data is in good agreement with the heat transfer data. determined using a state of the art liquid crystal heat distribution for the concave and convex surface was earlier for higher wake passing frequencies. In addition, found between TEXSTAN and the experimental data. Steady and frequency was observed to cause transition to occur sooner on in that they show that boundary layer transition occurs results of the heat transfer measurements. Extensive Stanton numbers predicted by TEXSTAN. Good agreement was surface due a separation bubble that induced transition for techniques. The results corroborate the heat transfer data the boundary layer transition behavior and corroborate the the concave surface. No effect was seen on the convex The effect of unsteady periodic wakes on heat transfer and the start and end of transition determined by the hot-wire transfer measurement technique. Higher wake passing tunnel facility. The local heat transfer coefficient unsteady boundary layer measurements were taken on the |
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| Item Description: | "Major subject: Mechanical Engineering". Vita. |
| Physical Description: | xiii, 162 leaves : illustrations ; 28 cm. Also available online. Issued also on microfiche from Lange Micrographics. |
| Bibliography: | Includes bibliographical references: pages 102-105. |