The effect of periodic-unsteady wakes, curvature, and pressure gradient on boundary-layer transition /
appeared to be classical Tollmien-Schhchting wave formations
| Main Author: | |
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| Format: | Thesis eBook |
| Language: | English |
| Published: |
[Place of publication not identified] :
[publisher not identified] ;
1994.
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| Subjects: | |
| Online Access: | Link to OAKTrust copy |
| Summary: | appeared to be classical Tollmien-Schhchting wave formations Boundary-layer transition on a concave curved plate has been cascade test facility with periodic-unsteady inlet flow was complete ensemble-averaged visualization of periodic-unsteady designed and manufactured for the next generation of research disturbance into the boundary-layer at the leading edge of generator. The transition procedure without wakes present in this area. independently convect downstream. Larninar regions were investigated with and without periodic-unsteady inlet flow at observed between wakes far beyond the streamwise position onset of transition over that of a zero pressure gradient. A periodic-unsteady wakes. In addition, a turbomachinery that were possibly modified by longitudinal Gbrtier vortices. the disturbance in the boundary-layer appeared to the plate. Afterwards, the wake strip in the free-stream and The presence of a negative pressure gradient delayed the they are confined to in the corresponding case without transition is also presented. The wake strip initiated a wakes were created using a rotating squirrel-cage type wake zero and negative pressure gradients. The periodicunsteady |
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| Item Description: | "Major subject: Mechanical Engineering". Vita. |
| Physical Description: | xii, 70 leaves : illustrations ; 28 cm. Also available online. |
| Bibliography: | Includes bibliographical references. |