EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF DIFFERENT CHEVRON NOZZLES /
שמור ב:
| מחבר ראשי: | |
|---|---|
| מחבר תאגידי: | |
| מחברים אחרים: | , |
| פורמט: | ספר |
| שפה: | אנגלית |
| יצא לאור: |
Dhaka :
AE DEPT. MIST,
c2026.
|
| נושאים: | |
| תגים: |
אין תגיות, היה/י הראשונ/ה לתייג את הרשומה!
|
פריטים דומים: 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 /