EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF DIFFERENT CHEVRON NOZZLES /
محفوظ في:
| المؤلف الرئيسي: | |
|---|---|
| مؤلف مشترك: | |
| مؤلفون آخرون: | , |
| التنسيق: | كتاب |
| اللغة: | الإنجليزية |
| منشور في: |
Dhaka :
AE DEPT. MIST,
c2026.
|
| الموضوعات: | |
| الوسوم: |
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
|
مواد مشابهة: EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF DIFFERENT CHEVRON NOZZLES /
- DESIGN AND COMPUTATIONAL ANALYSIS OF SUBSONIC LOITER MUNITION'S WING USING DIFFERENT AIRFOIL SECTION /
- ANALYZING AERO-STRUCTURAL BEHAVIOUR OF CONVENTIONAL AIRCRAFT WINGS THROUGH COMPUTATIONAL APPROACH AND EXPERIMENTAL VALIDATION /
- EXPERIMENTAL STUDY ON THE EFFECT OF DIFFERENT WINGLET CONFIGURATIONS ON THE LIFT AND DRAG CHARACTERISTICS OF A BLENDED WING BODY AIRCRAFT /
- SURFACE MODIFICATION OF NACA 4418 AIRFOIL WITH DIFFERENT SHAPED DIMPLES AND AERODYNAMIC PERFORMANCE ANALYSIS /
- EXPERIMENTAL STUDY OF MEAN FLOW CHARACTERISTICS OF SWIRLING JETS /
- EXPERIMENTAL STUDY OF FLOW AROUND A ROTATING CYLINDER /