Static Force Tests Of A Model Of A Twin Jet Fighter Airplane For Angles Of Attack From 10 Degrees To 110 Degrees And Sideslip Angles From 40 Degrees To 40 Degrees


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Aircraft Motion Sensitivity to Dynamic Stability Derivatives


Aircraft Motion Sensitivity to Dynamic Stability Derivatives

Author: T. F. Langham

language: en

Publisher:

Release Date: 1980


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A Collection of Technical Papers


A Collection of Technical Papers

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language: en

Publisher:

Release Date: 1977


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Naval Research Reviews


Naval Research Reviews

Author:

language: en

Publisher:

Release Date: 1976


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