Design of a normal acceleration limiting system for a high-performance aircraft

Bakemeyer, William F; Enders, William H

Design of a normal acceleration limiting system for a high-performance aircraft

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Author(s)

Bakemeyer, William F

•

Enders, William H

Advisor(s)

Robert C. Seamans, Jr.

Date Issued

1951

Publisher

Massachusetts Institute of Technology

Description

Thesis (M.S.) Massachusetts Institute of Technology. Dept. of Aeronautical Engineering, 1951.

Bibliography: leaves 72-73.

Subjects

Aeronautical Engineering Dept.

MIT Department

Massachusetts Institute of Technology. Department of Aeronautics and Astronautics

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