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University of Illinois at Urbana-Champaign
Mechanisms Controlling Non-Steady Plume-Wall Interactions in Rocket Launch-Tubes (Gas, Fluid Dynamics, Rocket Systems, Base Flows, Supersonic Flows)
Abstract
dc:descriptionThe mechanisms controlling the interactions between base flow induced irreversibilities with downstream effective critical flow conditions within rocket launch tubes due to friction and/or cross-sectional obstruction are studied here in detail. The analytical treatment by the flow component approach using one- and two-dimensional techniques is corroborated by a comprehensive experimental program.
Degree
thesis:*- Name thesis:degree_name
- Ph.D.
- Level thesis:degree_level
- Dissertation
- Discipline thesis:degree_discipline
- Mechanical Engineering
- Grantor
- University of Illinois at Urbana-Champaign
- Year dc:date
- 2014
Author and committee
dc:creator, dc:contributor.*- Author dc:creator
-
- Marongiu, Maurice Joseph
Subjects
dc:subject × 1Identifiers
dc:identifier.*- Identifier
- (UMI)AAI8600262
- OAI identifier oai:identifier
- oai:www.ideals.illinois.edu:2142/70133