The Application of Moving Wall Boundary Layer Control to Submarine Control Surfaces.
Final rept. 15 Jun 74-15 Jun 75,
TENNESSEE UNIV KNOXVILLE DEPT OF MECHANICAL AND AEROSPACE ENGINEERING
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This study involved the use of a moving wall for boundary layer control on submarine control surfaces. A rotating cylinder was applied at the leading edge, the trailing edge and at the body-flap junction of a control surface. Both analytical and experimental studies indicate that the maximum lift coefficient can be significantly increased in each of the three applications investigated.
- Submarine Engineering
- Fluid Mechanics