EFFECT OF THICKNESS-TO-CHORD RATIO ON AERODYNAMICS OF NONSLENDER DELTA WING


Thesis Type: Postgraduate

Institution Of The Thesis: Orta Doğu Teknik Üniversitesi, Faculty of Engineering, Department of Mechanical Engineering, Turkey

Approval Date: 2018

Student: MOHAMMAD SHARIFI GHAZIJAHANI

Supervisor: MEHMET METİN YAVUZ