A study of numerical methods to solve quasi one-dimensional, unsteady, compressible viscous flow with shock /
case, upon a McCormack predictor-corrector scheme are
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| Format: | Thesis eBook |
| Language: | English |
| Published: |
[Place of publication not identified] :
[publisher not identified] ;
1994.
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| Subjects: | |
| Online Access: | Link to OAKTrust copy |
| Summary: | case, upon a McCormack predictor-corrector scheme are consitions are considered, to simulate highly unsteady developed. Comparison between the inviscid flow and the flows. The advantages of this method, in this particular influence when the geometry of the nozzle is too large. internal flow in a subsonicsupersonic nozzle is obtained. inviscid and viscous flows, using an original two point Shocks due to high pressure ratio are computed for both subsonic-supersonic solving algorithm. Unsteady boundary The numerical simulation of a quasi one-dimensional viscous flow shows that the viscous effect have little |
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| Item Description: | "Major subject: Mechanical Engineering ". Vita. |
| Physical Description: | xiv, 137 leaves : illustrations ; 28 cm. Also available online. |
| Bibliography: | Includes bibliographical references. |