THERMO-MECHANICAL ANALYSIS OF AIRCRAFT STRUCTURES REINFORCED WITH STIFFENERS /
Wedi'i Gadw mewn:
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| Awdur Corfforaethol: | |
| Fformat: | Llyfr |
| Iaith: | Saesneg |
| Cyhoeddwyd: |
Dhaka :
AE DEPT. MIST,
c2025.
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| Pynciau: | |
| Tagiau: |
Dim Tagiau, Byddwch y cyntaf i dagio'r cofnod hwn!
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Eitemau Tebyg: THERMO-MECHANICAL ANALYSIS OF AIRCRAFT STRUCTURES REINFORCED WITH STIFFENERS /
- NATURAL FIBER REINFORCED POLYMER MATRIX COMPOSITES IN AIRCRAFT APPLICATION /
- THERMOMECHANICAL BEHAVIOR OF FIBER-REINFORCED COMPOSITE MATERIALS /
- A NUMERICAL STUDY ON THE OPTIMUM STRUCTURAL DESIGN OF AN AIRCRAFT TIRE TREAD /
- IMPROVING MECHANICAL PROPERTIES OF E-GLASS FIBER REINFORCED EPOXY COMPOSITES WITH FILLER MATERIALS /
- ANALYSIS OF OPERATIONAL LIMIT OF AN AIRCRAFT: AN AEROELASTIC APPROACH /
- ANALYZING AERO-STRUCTURAL BEHAVIOUR OF CONVENTIONAL AIRCRAFT WINGS THROUGH COMPUTATIONAL APPROACH AND EXPERIMENTAL VALIDATION /