Experimental investigation of the transient response in pitch of a helicopter

Mallen, Joseph

Experimental investigation of the transient response in pitch of a helicopter

Download

Name

29456305-MIT.pdf

Description

Full printable version

Size

9.49 MB

Format

Adobe PDF

Checksum (MD5)

036cb0cbc87761b7894791f9a433840b

Author(s)

Mallen, Joseph

Advisor(s)

R. H. Miller.

Date Issued

1949

Publisher

Massachusetts Institute of Technology

Description

Thesis (M.S.) Massachusetts Institute of Technology. Dept. of Aeronautical Engineering, 1949.

Includes bibliographies.

Subjects

Aeronautical Engineering Dept.

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/1721.1/67130