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

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Détails bibliographiques
Auteur principal:	Sorker, Md. Sohan
Collectivité auteur:	Supervised by Air Cdre Md. Abdus Salam (Instructor, Dept. of Aeronautical Engineering., MIST, DHAKA.)
Autres auteurs:	Md. Sohan Sorker, Md. Tariqul Islam, Shakil Mahmud
Format:	Livre
Langue:	anglais
Publié:	Dhaka : AE DEPT MIST , C 2018.
Sujets:	Thesis Paper of AE in B.Sc Prog. Aeronautical Engineering.
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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.
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