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

में बचाया:

ग्रंथसूची विवरण
मुख्य लेखक:	Sorker, Md. Sohan
निगमित लेखक:	Supervised by Air Cdre Md. Abdus Salam (Instructor, Dept. of Aeronautical Engineering., MIST, DHAKA.)
अन्य लेखक:	Md. Sohan Sorker, Md. Tariqul Islam, Shakil Mahmud
स्वरूप:	पुस्तक
भाषा:	अंग्रेज़ी
प्रकाशित:	Dhaka : AE DEPT MIST , C 2018.
विषय:	Thesis Paper of AE in B.Sc Prog. Aeronautical Engineering.
टैग:	टैग जोड़ें कोई टैग नहीं, इस रिकॉर्ड को टैग करने वाले पहले व्यक्ति बनें!

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

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