Numerical investigations of scarmjet unstart

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Abstract/Contents

Abstract
Supersonic combusting ramjets (scramjets) have been envisioned as an economic means for long-range hypersonic delivery system and access to outer space. If strong disturbances such as those due to combustion occur in the engine, a failure mode called unstart could result. When unstart occurs, the mass flow rate through the engine inlet cannot be maintained, leading to loss-of-thrust and engine stall. Because the probability of unstart grows with increasing heat release from combustion, the danger of unstart is an important factor limiting the performance of scramjets. The present studies perform calculations of scramjet unstart in both cold and hot airflows based on Reynolds-averaged Navier-Stokes (RANS) turbulence closures. The flow solver is first validated against a Mach 5 experiment without combustion, aiming at establishing confidence in the unstart-prediction capability of the solver. Modifications to the solver are then proposed to improve its convergence rate to steady-state solutions and to provide tools for the analysis of unstart dynamics. Finally, the solution curve of a Mach 8 scramjet is calculated in a wide range of heat-release rates in conjunction with studies of the bifurcation structure of scramjet systems. We will also discuss linearized system dynamics that provide insight into a metric to forewarn unstart and unstart-mitigation mechanisms.

Description

Type of resource text
Form electronic; electronic resource; remote
Extent 1 online resource.
Publication date 2016
Issuance monographic
Language English

Creators/Contributors

Associated with Jang, Ik
Associated with Stanford University, Department of Mechanical Engineering.
Primary advisor Moin, Parviz
Thesis advisor Moin, Parviz
Thesis advisor Alonso, Juan José, 1968-
Thesis advisor Lele, Sanjiva K. (Sanjiva Keshava), 1958-
Advisor Alonso, Juan José, 1968-
Advisor Lele, Sanjiva K. (Sanjiva Keshava), 1958-

Subjects

Genre Theses

Bibliographic information

Statement of responsibility Ik Jang.
Note Submitted to the Department of Mechanical Engineering.
Thesis Thesis (Ph.D.)--Stanford University, 2016.
Location electronic resource

Access conditions

Copyright
© 2016 by Ik Jang
License
This work is licensed under a Creative Commons Attribution Non Commercial 3.0 Unported license (CC BY-NC).

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