Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1997-05-09
2000-10-03
Poon, Peter M.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
B64C 2306
Patent
active
061261181
ABSTRACT:
A flow separation reducer comprises a vane which prevents an airflow from being separated in a flow interference region where a plurality of members, such as a main wing and a pylon, are joined to each other. The vane is disposed in a location where the airflow along a surface of one of the members develops a minimum negative pressure. The vane has a predetermined angle of attack with respect to the airflow for generating a vortex downstream of the vane with respect to the airflow and causing a circulation around the vane to reduce the speed of the airflow in the location.
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Fujino Michimasa
Kawamura Yuichi
Honda Giken Kogyo Kabushiki Kaisha
Palo Francis T.
Poon Peter M.
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