MECHANICAL DESIGN AND MATERIAL CHARACTERIZATION OF ADDIVITIVELY MANUFACTURED TI6AL4V CONTROL SURFACE FOR AN AERO VEHICLE USING SELECTIVE LASER MELTING TECHNIQUE / (Record no. 610555)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 02361nam a22001577a 4500 |
| 082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER | |
| Classification number | 621 |
| 100 ## - MAIN ENTRY--PERSONAL NAME | |
| Personal name | Shah, Syed Waqas Ali |
| 245 ## - TITLE STATEMENT | |
| Title | MECHANICAL DESIGN AND MATERIAL CHARACTERIZATION OF ADDIVITIVELY MANUFACTURED TI6AL4V CONTROL SURFACE FOR AN AERO VEHICLE USING SELECTIVE LASER MELTING TECHNIQUE / |
| Statement of responsibility, etc. | Syed Waqas Ali Shah |
| 264 ## - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE | |
| Place of production, publication, distribution, manufacture | Islamabad : |
| Name of producer, publisher, distributor, manufacturer | SMME- NUST; |
| Date of production, publication, distribution, manufacture, or copyright notice | 2024. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Extent | 95p. |
| Other physical details | Soft Copy |
| Dimensions | 30cm |
| 500 ## - GENERAL NOTE | |
| General note | The 3D printing of metals from power is an emerging technology in the field of material and<br/>manufacturing producing complex shape light weight geometries directly from design data.<br/>Selective laser melting is one of the promising additive manufacturing techniques for providing<br/>near net shape, less material waste, short leading time, and low cost. Ti6Al4V serves as a great<br/>material of choice for this manufacturing technique and provides an excellent combination of<br/>properties in aerospace structures because of lightweight, high strength, corrosion resistance and<br/>high service temperatures. The aim of this project is to design and optimize control surface and<br/>additively manufactured it from Ti6Al4V alloy using Selective laser melting technique. Also, to<br/>characterize the material properties of SLMed printed Ti6Al4V alloy to measure thermal and<br/>mechanical properties and their comparison with traditional manufactured products mentioned in<br/>MIL-HDBK standard. Samples are printed and tested on UTM to measure yield strength, tensile<br/>strength, Young`s Modulus and percentage elongation at room temperature and at elevated<br/>temperatures up to 600C0<br/>. The tensile strength dropped by 67% from room temperature to 600C0<br/>.<br/>A 3-point bending test is conducted to measure critical Bending strength, Flexural Modulus, and<br/>stress intensity factor. Thermal Conductivity is measured by GHFM up to 300C0<br/>. coefficient of<br/>thermal expansion and specific heat is measured up to 600C0<br/>by dilatometer and scanning<br/>calorimeter respectively. All these results are compared with traditional manufactured parts<br/>concluded that SLMed products can be used for the same strength and application with less cost,<br/>material, and time. |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | MS Mechanical Engineering |
| 700 ## - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Supervisor : Dr. Sadaqat Ali |
| 856 ## - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | <a href="http://10.250.8.41:8080/xmlui/handle/123456789/44880">http://10.250.8.41:8080/xmlui/handle/123456789/44880</a> |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Source of classification or shelving scheme | |
| Koha item type | Thesis |
| Withdrawn status | Permanent Location | Current Location | Shelving location | Date acquired | Full call number | Barcode | Koha item type |
|---|---|---|---|---|---|---|---|
| School of Mechanical & Manufacturing Engineering (SMME) | School of Mechanical & Manufacturing Engineering (SMME) | E-Books | 07/24/2024 | 621 | SMME-TH-1030 | Thesis |