Immunity-based flight envelope prediction at post-failure conditions
نویسندگان
چکیده
منابع مشابه
Stress Analysis of Flight Vehicles under Flight Conditions
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A method is presented for the stress analysis of flight vehicles under different flight conditions including gust and control surface deflection (or maneuver) using the governing equations of rigid-body motions and elastic deformations. The Lagrangian approach is used to derive the governing equations of motions. For this purpose, the basic equations of motions are derived in terms of potential...
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ژورنال
عنوان ژورنال: Aerospace Science and Technology
سال: 2015
ISSN: 1270-9638
DOI: 10.1016/j.ast.2015.07.014