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- W2356771716 abstract "In order to strengthen maneuverability of fighter aircrafts and decrease rader wave reflection a tailless fighter aircraft has become one of new research directions.The research work discussed in this paper is based on the background of yawing control project of the tailless fighter.The fineness of the model bodies tested is 5.2.The section shapes of the models are circle,elliptic and elliptic section with a sharp edge,which is similar to the section of the nose of the tailless airplane.The flow phenomenon,especially asymmetric one,over different bodies were investigated at angles of attack ranging from 0° to 90° in a water tunnel.Measurement of forces was performed in a wind tunnel.Test results show that side force change of the cone-cylinder body is very large.The body with the sharp edge has minimum side force compared with other two configurations of body." @default.
- W2356771716 created "2016-06-24" @default.
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- W2356771716 date "2006-01-01" @default.
- W2356771716 modified "2023-09-28" @default.
- W2356771716 title "Investigation of asymmetric flow pattern and side force of slender forebodies with different cross sections" @default.
- W2356771716 hasPublicationYear "2006" @default.
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