http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY LAYER CONTROL ( MSBC) ON SINGLE & DOUBLE CYLINDER CONFIGURATION NACA 23018 AIRFOIL
Instructor, Dept. of Aeronautical Engineering., MIST, DHAKA.
Md. Sohan Sorker, Md. Tariqul Islam, Shakil Mahmud.