Simulation and Analysis for Aerodynamic Characteristics of Flying Object Based on Canard

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Abstract:

Change the aerodynamic characteristics of the flying object by controlling the canard deflection and achieve ballistic correction of the flying object. Select different angles of attack to simulate and analyze the changes on aerodynamic performance of the flying object at different flight speed. Study the variation regularity and influence factors of aerodynamic characteristics with the deflection angle and the area of the canard as characteristic parameters.

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415-420

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October 2011

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© 2012 Trans Tech Publications Ltd. All Rights Reserved

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