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  • The computational model was applied for investigation of the dynamic stability with six degrees of freedom at real aeroplane, where the mutual very strong aerodynamic couplings of longitudinal and lateral-directional motions, caused by the interference between wing and fuselage, were demonstrated by the results from the wind-tunnel tests.
  • The computational model was applied for investigation of the dynamic stability with six degrees of freedom at real aeroplane, where the mutual very strong aerodynamic couplings of longitudinal and lateral-directional motions, caused by the interference between wing and fuselage, were demonstrated by the results from the wind-tunnel tests. (en)
Title
  • Analysis of aeroplane dynamic stability with six degree of freedom
  • Analysis of aeroplane dynamic stability with six degree of freedom (en)
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  • Analysis of aeroplane dynamic stability with six degree of freedom
  • Analysis of aeroplane dynamic stability with six degree of freedom (en)
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  • RIV/00216305:26210/02:PU36065!RIV11-MSM-26210___
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  • 638042
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  • RIV/00216305:26210/02:PU36065
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  • Aeronautics, Aeroplane, Flight Mechanics, Dynamic stability (en)
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  • [DF27E9D68171]
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  • Vilnius Lithuania
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  • Vilnius Lithuania
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  • Recent Research and Design Progress in Aeronautical Engineering and its Influence on Education. Book of Abstracts
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  • Daněk, Vladimír
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  • Vilniaus Gedimino Technikos Universitetas
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  • 9986-05-571-7
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  • 26210
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