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University of Petroleum and Energy Studies (UPES)
Department of Aerospace Engineering
Computational Investigation of the Effect of Nose mounted Devices on the Aerothermodynamics of a Missile Shaped Body Flying at Hypersonic Speeds
Computational Investigation of the Effect of Nose mounted Devices on the Aerothermodynamics of a Missile Shaped Body Flying at Hypersonic Speeds
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01_title.pdf
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02_certificate.pdf
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03_summary.pdf
(30.27 KB)
04_declaration.pdf
(10.82 KB)
05_acknowledgement.pdf
(8.25 KB)
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http://hdl.handle.net/10603/183654
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Department of Aerospace Engineering
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