S. YAYLA Et Al. , "The effect of angle of attack on the flow structure over the nonslender lambda wing," AEROSPACE SCIENCE AND TECHNOLOGY , vol.28, no.1, pp.417-430, 2013
YAYLA, S. Et Al. 2013. The effect of angle of attack on the flow structure over the nonslender lambda wing. AEROSPACE SCIENCE AND TECHNOLOGY , vol.28, no.1 , 417-430.
YAYLA, S., CANPOLAT, Ç., ŞAHİN, B., & AKILLI, H., (2013). The effect of angle of attack on the flow structure over the nonslender lambda wing. AEROSPACE SCIENCE AND TECHNOLOGY , vol.28, no.1, 417-430.
YAYLA, Sedat Et Al. "The effect of angle of attack on the flow structure over the nonslender lambda wing," AEROSPACE SCIENCE AND TECHNOLOGY , vol.28, no.1, 417-430, 2013
YAYLA, Sedat Et Al. "The effect of angle of attack on the flow structure over the nonslender lambda wing." AEROSPACE SCIENCE AND TECHNOLOGY , vol.28, no.1, pp.417-430, 2013
YAYLA, S. Et Al. (2013) . "The effect of angle of attack on the flow structure over the nonslender lambda wing." AEROSPACE SCIENCE AND TECHNOLOGY , vol.28, no.1, pp.417-430.
@article{article, author={Sedat YAYLA Et Al. }, title={The effect of angle of attack on the flow structure over the nonslender lambda wing}, journal={AEROSPACE SCIENCE AND TECHNOLOGY}, year=2013, pages={417-430} }