New General Approach to Airplane Rotation Analysis
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- BAJOVIC Milan
- Aeronautical Institute
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- ZIVANOVIC Milovan
- Mihailo Pupin Institute
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- RASUO Bosko
- Faculty of Mechanical Engineering, University of Belgrade
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- STOJAKOVIC Predrag
- Aeronautical Institute
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Abstract
The paper presents a new approach to analysis of dynamic properties of the rotating airplane. The analysis is based on the rate of rotational energy and a full non-linear model of airplane dynamics. It can be applied to a whole range of attack angles. To provide stable rotation, it is sufficient to use algebra and know only the inertial properties of the airplane and the functional relations of either aerodynamic moments or angular accelerations. We prove that the results are fully congruent with those obtained by conventional methods within the scope of validity of the simplified model.
Journal
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 53 (180), 130-137, 2010
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390282679057082496
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- NII Article ID
- 10026613059
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- NII Book ID
- AA0086707X
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- ISSN
- 21894205
- 05493811
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- NDL BIB ID
- 10782807
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- Text Lang
- en
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed