Roll control reversal of variable swept wing in supersonic flow
Roll control reversal of a variable swept wing is investigated in the present paper. The wing model is based on the Rodden-Love forward swept wing which is modified in the present work so that it can swept forward and backward. The flexural and torsional wing flexibilities are considered in the...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English English |
| Published: |
Blue Eyes Intelligence Engineering & Sciences Publication
2019
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/73130/7/73130%20Roll%20control%20reversal%20of%20variable.pdf http://irep.iium.edu.my/73130/8/73130%20Roll%20control%20reversal%20of%20variable%20SCOPUS.pdf http://irep.iium.edu.my/73130/ https://www.ijrte.org/wp-content/uploads/papers/v7i6s/F02550376S19.pdf |
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| Institution: | Universiti Islam Antarabangsa Malaysia |
| Language: | English English |
| Summary: | Roll control reversal of a variable swept wing is
investigated in the present paper. The wing model is based on
the Rodden-Love forward swept wing which is modified in the
present work so that it can swept forward and backward. The
flexural and torsional wing flexibilities are considered in the
analysis so that their influence on the aileron control
effectiveness can be assessed. The influence of the vertical tail
is included in the trim analysis in several flight altitudes. A
parametric study by varying the wing bending and torsional
stiffness is conducted. The result shows that the aileron
control effectiveness of the forward swept wing performs
better than the backward swept wing for the present model. |
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