Enhanced compressor distortion tolerance using asymmetric inlet guide vane stagger

Schulmeyer, Andreas

Enhanced compressor distortion tolerance using asymmetric inlet guide vane stagger

Download

Name

22140692-MIT.pdf

Description

Full printable version

Size

2.62 MB

Format

Adobe PDF

Checksum (MD5)

2037c792d11f32f7879d997e9baba690

Author(s)

Schulmeyer, Andreas

Date Issued

1989

Publisher

Massachusetts Institute of Technology

Description

Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.

GRSN 406823

Includes bibliographical references (leaf 37).

Subjects

Aeronautics and Astronautics.

MIT Department

Massachusetts Institute of Technology. Department of Aeronautics and Astronautics

Terms of Use

M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.

http://dspace.mit.edu/handle/1721.1/7582

Persistent DSpace Link

http://hdl.handle.net/1721.1/40144