Old Web
English
Sign In
Acemap
>
Paper
>
PREDICTION OF AERODYNAMIC COEFFICIENTS OF A SUPERSONIC WING USING BOUNDARY ELEMENT METHOD
PREDICTION OF AERODYNAMIC COEFFICIENTS OF A SUPERSONIC WING USING BOUNDARY ELEMENT METHOD
2009
Hossein Shahverdi
M H Dolabi
M Behbahani Nejad
Keywords:
Supersonic speed
Aerodynamics
Boundary element method
Choked flow
Physics
Wing
Aerospace engineering
Correction
Source
Cite
Save
Machine Reading By IdeaReader
0
References
0
Citations
NaN
KQI
[]