STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY LAYER CONTROL ( MSBC) ON SINGLE & DOUBLE CYLINDER CONFIGURATION NACA 23018 AIRFOIL /

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Bibliografische gegevens
Hoofdauteur: Sorker, Md. Sohan
Coauteur: Supervised by Air Cdre Md. Abdus Salam (Instructor, Dept. of Aeronautical Engineering., MIST, DHAKA.)
Andere auteurs: Md. Sohan Sorker, Md. Tariqul Islam, Shakil Mahmud
Formaat: Boek
Taal:Engels
Gepubliceerd in: Dhaka : AE DEPT MIST , C 2018.
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LEADER 00000nam a22000007a 4500
001 TP-1356
003 BD-DhMIS
005 20191013125630.0
008 191013b xxu||||| |||| 00| 0 eng d
040 |a BD-DhMIS   |c BD-DhMIS  
100 |a Sorker, Md. Sohan , 
245 |a STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY LAYER CONTROL ( MSBC) ON SINGLE & DOUBLE CYLINDER CONFIGURATION NACA 23018 AIRFOIL /  |c Md. Sohan Sorker, Md. Tariqul Islam, Shakil Mahmud. 
260 |a Dhaka :  |b AE DEPT MIST ,  |c C 2018. 
300 |a 154. :  |b ill. ;  |c 29 cm. 
541 |e TP-1356 
650 |a Thesis Paper of AE in B.Sc Prog. 
650 |a Aeronautical Engineering. 
700 |a Md. Sohan Sorker,  
700 |a Md. Tariqul Islam,  
700 |a Shakil Mahmud. 
710 |a Supervised by Air Cdre Md. Abdus Salam.  |e Instructor, Dept. of Aeronautical Engineering., MIST, DHAKA. 
942 |2 ddc  |c TP 
999 |c 7581  |d 7581