Flow-induced vibrations of low aspect ratio rectangular membrane wings

MS Genc - Journal of Fluids and Structures, 2011 - Elsevier
An experimental study of a low aspect ratio rectangular membrane wing in a wind tunnel
was conducted for a Reynolds number range of 2.4× 104–4.8× 104. Time-accurate …
被引用次数：137 相关文章
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[PDF][PDF] Flow-induced vibrations of low aspect ratio rectangular membrane wings

P Rojratsirikul, MS Genc, Z Wang, I Gursul - Journal of Fluids and …, 2011 - core.ac.uk
An experimental study of a low aspect ratio rectangular membrane wing in a wind tunnel
was conducted for a Reynolds number range of 2.4 x10 4 to 4.8 x10 4. Time-accurate …

[引用][C] Flow-induced vibrations of low aspect ratio rectangular membrane wings

P ROJRATSIRIKUL, MS GENC… - Journal of fluids and …, 2011 - pascal-francis.inist.fr
Flow-induced vibrations of low aspect ratio rectangular membrane wings CNRS Inist Pascal-Francis
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Flow-induced vibrations of low aspect ratio rectangular membrane wings

P Rojratsirikul, M Genc, Z Wang… - Journal of Fluids and …, 2011 - avesis.erciyes.edu.tr
An experimental study of a low aspect ratio rectangular membrane wing in a wind tunnel
was conducted for a Reynolds number range of 2.4× 104-4.8× 104. Time-accurate …

Flow-induced vibrations of low aspect ratio rectangular membrane wings

P Rojratsirikul, MS Genc, Z Wang… - Journal of Fluids and …, 2011 - researchportal.bath.ac.uk
An experimental study of a low aspect ratio rectangular membrane wing in a wind tunnel
was conducted for a Reynolds number range of 2.4104-4.8104. Time-accurate …

Flow-induced vibrations of low aspect ratio rectangular membrane wings

P Rojratsirikul, MS Genc, Z Wang… - Journal of Fluids and …, 2011 - ui.adsabs.harvard.edu
An experimental study of a low aspect ratio rectangular membrane wing in a wind tunnel
was conducted for a Reynolds number range of 2.4× 10 4-4.8× 10 4. Time-accurate …

Flow-induced vibrations of low aspect ratio rectangular membrane wings

P Rojratsirikul, MS Genc, Z Wang, I Gursul - 2011 - aperta.ulakbim.gov.tr
An experimental study of a low aspect ratio rectangular membrane wing in a wind tunnel
was conducted for a Reynolds number range of 2.4 x 10 (4)-4.8 x 10 (4). Time-accurate …

Flow-induced vibrations of low aspect ratio rectangular membrane wings

P Rojratsirikul, MS Genc, Z Wang, I Gursul - Journal of Fluids and …, 2011 - infona.pl
An experimental study of a low aspect ratio rectangular membrane wing in a wind tunnel
was conducted for a Reynolds number range of 2.4× 10 4–4.8× 10 4. Time-accurate …

Flow-induced vibrations of low aspect ratio rectangular membrane wings

P Rojratsirikul, M Genc, Z Wang… - Journal of Fluids and …, 2011 - avesis.erciyes.edu.tr
An experimental study of a low aspect ratio rectangular membrane wing in a wind tunnel
was conducted for a Reynolds number range of 2.4× 104-4.8× 104. Time-accurate …

Flow-induced vibrations of low aspect ratio rectangular membrane wings

P Rojratsirikul, MS Genc, Z Wang, I Gursul - 2011 - aperta.ulakbim.gov.tr
An experimental study of a low aspect ratio rectangular membrane wing in a wind tunnel
was conducted for a Reynolds number range of 2.4 x 10 (4)-4.8 x 10 (4). Time-accurate …