What you will learn
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This course is expected to impart firsthand knowledge of compressible flows as it applies to both the supersonic and hypersonic Mach number regimes. It combines the theoretical approach with the numerical one without making it too detailed and intricate. After successful completion of this course the student should be well prepared for more advanced courses in the discipline. With ever increasing use of high speed flows in a wide gamut of applications, especially in the defence and space sectors, it is essential to understand the basic concepts of compressible flows over a wide Mach number range while working on any of the above applications. This course exactly fulfils that need. Applications of shock waves in other disciplines is also discussed briefly in this course. I would like to once more emphasize that the primary intention of this course is to create a familiarity about the supersonic and hypersonic flow regimes. It is not intended to prepare someone for research but induce the excitement and enthusiasm to pursue it further.
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Meet Your Instructor
About Instructor
VTU is one of the largest Technological Universities in India with 24 years of Tradition of excellence in Engineering & Technical Education, Research and Innovations. It came into existence in the year 1998 to cater the needs of Indian industries for trained technical manpower with practical experience and sound theoretical knowledge.
Free
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Course Duration31 h 4 m 49 s
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Course LevelIntermediate
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Student Enrolled0
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LanguageEnglish
This Course Includes
- 31 h 4 m 49 s Video Lectures
- 0 Quizzes
- 0 Assignments
- 0 Downloadable Resources
- Full Lifetime Access
- Certificate of Completion