A Higher Order Panel Method With Source and Doublet Continuity to Calculate The Areodynamic Characteristics of a Supersonic Wing
Author name:
Yaseen Taha Mohammed Al-Sheet
Supervisor name:
A. A. Al-Sudani | As. K. Darwish
General topic:
Mechanical Engineering
Specific topic:
Fluid Dynamics
Degree:
Master
University:
University of Technology - Department Of Mechanical Engineering
Language:
English
University location:
Baghdad
First pages:
T93333 - p.pdf
