Aerothermodynamic cycle analysis of a dual-spool, separate-exhaust turbofan engine with an interstage turbine burner

Liew, Ka Heng

Back to search

Michigan Technological University

Aerothermodynamic cycle analysis of a dual-spool, separate-exhaust turbofan engine with an interstage turbine burner

dc:creator Liew, Ka Heng

thesis:degree_name Doctor of Philosophy in Mechanical Engineering-Engineering Mechanics (PhD)

Degree

thesis:*

Name thesis:degree_name: Doctor of Philosophy in Mechanical Engineering-Engineering Mechanics (PhD)
Level thesis:degree_level: Dissertation

Author and committee

dc:creator, dc:contributor.*

Author dc:creator: Liew, Ka Heng
Contributors dc:contributor: Song-Lin Yang

Subjects

dc:subject × 2

Identifiers

dc:identifier.*

Identifier: https://digitalcommons.mtu.edu/etds/382
OAI identifier oai:identifier: oai:digitalcommons.mtu.edu:etds-1381

Chain of custody

source

Harvested from: Michigan Technological University
Base URL: digitalcommons.mtu.edu/do/oai/
Last updated: 2026-07-27
Source record: OAI-PMH GetRecord

related terms

citation

Liew, Ka Heng. Aerothermodynamic cycle analysis of a dual-spool, separate-exhaust turbofan engine with an interstage turbine burner. Dissertation thesis, https://doi.org/10.37099/mtu.dc.etds/382

Aerothermodynamic cycle analysis of a dual-spool, separate-exhaust turbofan engine with an interstage turbine burner

Degree

Author and committee

Subjects

Identifiers

Chain of custody

More from Michigan Technological University