| Type of Material: | Thesis |
| Title: | Active flow control for hypersonic flows involving real gas and magnetohydrodynamic effects |
| Researcher: | Balasubramanian R. |
| Guide: | Anandhanarayanan K. |
| Department: | Department of Mechanical Engineering |
| Publisher: | Jawaharlal Nehru Technological University, Hyderabad |
| Place: | Hyderabad |
| Year: | 2016 |
| Language: | English |
| Subject: | Engineering | Engineering and Technology | Engineering Mechanical | Flight vehicle | Hypersonic flows | Mechanical engineering | Engineering and Technology |
| Dissertation/Thesis Note: | PhD; Department of Mechanical Engineering, Jawaharlal Nehru Technological University, Hyderabad, Hyderabad; 2016 |
| Fulltext: | Shodhganga |
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| 040 | __ | |aJNTU_500028|dIN-AhILN |
| 041 | __ | |aeng |
| 100 | __ | |aBalasubramanian R.|eResearcher |
| 110 | __ | |aDepartment of Mechanical Engineering|bJawaharlal Nehru Technological University, Hyderabad|dHyderabad|ein|0U-0017 |
| 245 | __ | |aActive flow control for hypersonic flows involving real gas and magnetohydrodynamic effects |
| 260 | __ | |aHyderabad|bJawaharlal Nehru Technological University, Hyderabad|c2016 |
| 300 | __ | |a327p.|dDVD |
| 502 | __ | |cDepartment of Mechanical Engineering, Jawaharlal Nehru Technological University, Hyderabad, Hyderabad|d2016|bPhD |
| 518 | __ | |dMay 2016|oDate of Award |
| 518 | __ | |oDate of Registration|d2008-01-01 |
| 520 | __ | |aActive flow control of hypersonic flight vehicle forms a crucial design requirement for hypersonic research and technology development. Aerodynamic and propulsive controls are the two main affiliates of flow control to be achieved during flight. The flight vehicle can be a projectile, a re-entry payload, a cruise missile or an air-breathing hypersonic scramjet cruise vehicle (HSCV). Active flow control of HSCV is considered the most challenging due to complexities associated with direct coupling of hypervelocity aerodynamic and propulsive flow characteristics. For successful operation and completion of mission objectives of HSCV right from launch phase to touch-down, active flow controls which utilize new multidisciplinary and evolutionary physical mechanisms, such as electromagnetic flow control and plasma discharge flow control are required during the flight. Due to the complex interaction of electromagnetic field and chemically reacting ionized flow field, the flowfield analysis needs to consider sophist |
| 650 | __ | |aMechanical engineering|2UGC |
| 650 | __ | |aEngineering and Technology|2AIU |
| 653 | __ | |aEngineering |
| 653 | __ | |aEngineering and Technology |
| 653 | __ | |aEngineering Mechanical |
| 653 | __ | |aFlight vehicle |
| 653 | __ | |aHypersonic flows |
| 700 | __ | |eGuide|aAnandhanarayanan K. |
| 856 | __ | |uhttp://shodhganga.inflibnet.ac.in/handle/10603/292961|yShodhganga |
| 905 | __ | |afromsg |
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