Parametric Analysis of a Hypersonic Inlet using Computational Fluid Dynamics

Parametric Analysis of a Hypersonic Inlet using Computational Fluid Dynamics

abstract: For CFD validation, hypersonic flow fields are simulated and compared with experimental data specifically designed to recreate conditions found by hypersonic vehicles. Simulated flow fields on a cone-ogive with flare at Mach 7.2 are compared with experimental data from NASA Ames Research C...

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Bibliographic Details
Other Authors: Oliden, Daniel Oscar (Author)
Format: Dissertation
Language:English
Published: 2013
Subjects:
Aerospace engineering
aerothermodynamics
cfd
computational
fluent
hypersonic
inlet
Online Access:http://hdl.handle.net/2286/R.I.20879

Internet

http://hdl.handle.net/2286/R.I.20879

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