Flight vibration survey of F-106A aircraft /
H. Kent Reich.

Description

Main Author

Reich, H. Kent.

Related Names

United States. Air Force.

Language(s)

English

Published

Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962.

Subjects

Vibration > Vibration / Measurement > Vibration / Measurement / Instruments.
Vibration (Aeronautics)
Fighter planes.

Summary

An F-106A aircraft was surveyed to determined the vibration environment existing throughout the vehicle under all flight conditions expected in service. Approximately 18,890 data points were obtained from 25 separate locations on the vehicle during 23 test flights. The data obtained were evaluated to determine the adequacy of vibration test requirements for aircraft equipment as contained in Specification No. Mil-E-5272C. The data indicated that the vibration testing requirements of the specification are more than adequate, a finding substantiated by all previous (vibration) surveys performed on Century Series aircraft.

Note

"AD0282207 (from http://www.dtic.mil)."
"May 1962."

Physical Description

xiii, 37 pages : illustrations, figures ; 28 cm.

Locate a Print Version

Find in a library

Viewability