Effect of spikes integrated to airfoil at supersonic speed
Master_Thesis_Koushik
1. Master thesis report on
VORTEX SHEDDING AND AERODYNAMIC DRAG ON TRUNCATED
TRAILING EDGE AIRFOIL
Conducted during
February - June 2015
Submitted by:
Koushik Bangalore Gangadharacharya
Master of Science in Aerospace Engineering
Royal Institute of Technology, Stockholm, Sweden
Under the supervision of
Hans Mårtensson&Lars Ellbrant
GKN Aerospace, Trollhättan, Sweden
Examiner:
Prof. Arthur Rizzi
Aeronautical and Vehicle Engineering Dept.
Royal Institute of Technology, Stockholm, Sweden.