STUDENT ANALYSIS OF AIRCRAFT WINGS WITH VARIOUS CONDITIONS /
محفوظ في:
| المؤلف الرئيسي: | |
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| مؤلف مشترك: | |
| مؤلفون آخرون: | , , |
| التنسيق: | كتاب |
| اللغة: | الإنجليزية |
| منشور في: |
Dhaka :
AE DEPT MIST ,
C 2015 .
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| الموضوعات: | |
| الوسوم: |
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
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مواد مشابهة: STUDENT ANALYSIS OF AIRCRAFT WINGS WITH VARIOUS CONDITIONS /
- STRUCTURAL ANALYSIS OF AIR CRAFT WINGS WITH VARIOUS CONDITIONS /
- LARGE DEFECTION ANALYSIS OF AN AIRCRAFT WING WITH ELLIPTICAL LIFT DISTRIBUTION AT DIFFERENT FLIGHT CONDITION /
- PERFORMANCE OPTIMIZATION OF A VARIABLE GEOMETRICAL WING:ANALYSIS AND DESIGN OF MORPHING WING FOR UNMANNED AERIAL VEHICLE /
- DESIGN & FABRICATION OF WING CONTROLS,UNDERCARRIAGE AND SKIN OF HOME BUILT EXPERIMENTAL AIRCRAFT’’ MIST X-01’’ /
- PROPERTIES OF NATURAL POLYMER MATRIX COMPOSITE WITH VARIOUS FIBER ORIENTATIONS /
- PASSIVE CONTROL OF WING ROCK IN A DELTA WING AIRCRAFT /