Invention Application
- Patent Title: DIVERGENT TRAILING-EDGE AIRFOIL
- Patent Title (中): 潜水拖车边缘航空
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Application No.: PCT/US1987003260Application Date: 1987-12-08
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Publication No.: WO1988009745A1Publication Date: 1988-12-15
- Inventor: MCDONNELL DOUGLAS CORPORATION , HENNE, Preston, A. , GREGG, Robert, D., III
- Applicant: MCDONNELL DOUGLAS CORPORATION
- Assignee: MCDONNELL DOUGLAS CORPORATION
- Current Assignee: MCDONNELL DOUGLAS CORPORATION
- Priority: US56,250 19870601
- Main IPC: B64C03/14
- IPC: B64C03/14
Abstract:
A special contour near the trailing edge (24) of an airfoil (20) which improves the airfoil effectiveness. The contour is a combination of a blunt airfoil base (28), a local region of high surface curvature, typically on the airfoil lower surface, and upper surface and lower surface trailing edge slopes that diverge from each other (30).
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