University of Tasmania
Browse

File(s) not publicly available

BOUNDARY LAYER DEVELOPMENT IN AXIAL COMPRESSORS AND TURBINES. PART 4 OF 4: COMPUTATIONS & ANALYSES

conference contribution
posted on 2023-05-23, 02:18 authored by Halstead, DE, Wisler, DC, Okiishi, TH, Walker, GJ, Hodson, HP, Shin, HW
No description available

History

Volume

ASME Paper 95-GT-464

Pagination

1-16

Department/School

School of Engineering

Publisher

The American Society of Mechanical Engineers

Event title

International Gas Turbine and Aeroengine Congress and Exposition

Event Venue

Houston, Texas, U.S.A.

Date of Event (Start Date)

1995-01-01

Date of Event (End Date)

1995-01-01

Repository Status

  • Restricted

Socio-economic Objectives

Expanding knowledge in philosophy and religious studies

Usage metrics

    University Of Tasmania

    Categories

    Keywords

    No keyword provided

    Licence

    In Copyright

    Exports

    RefWorks
    BibTeX
    Ref. manager
    Endnote
    DataCite
    NLM
    DC