AC 23.629-1A

Historical

Advisory circular · Means of Compliance with Section 23.629, "Flutter"

A newer version is currentThis is a historical version. AC 23.629-1B is the version in force, approved September 28, 2004.
Approved
October 23, 1985
Last reviewed
August 13, 2001
Cancelled by
AC23.629-1B
Family
AC 23.629-1 · 2 versions
Revision
A
14 CFR parts
23
14 CFR sections
§ 23.629

Guidance, not mandatory unless a rule or AD requires it. DRS record last changed November 22, 2025.

Show pages 40–51

Appendix 4 BIBLIOGRAPHY:

1. Manual on Aeroelasticity, North Atlantic Teaty Organization Advisory Group for Aeronautical Research and Development (AGARD).

2. Analytical Methods in Vibration. Mierovetch, McMillan Company, New York, 1967.

3. An Introduction to the Theory of Aeroelasticity, Fung, John Wiley and Co., New York, 1955.

4. Dynamics of Structures, Hurty and Rubinstein, Prentice-Hall, New York, 1964.

5. Sane Aspects of Ground and Flight Vibration Tests, Mazet, ONERA TN No.

34, 1956.

6. A Survey of Aircraft Subcritical Flight Flutter Testing Methods, Rosenbaum, A.R.A.P. Report No. 218, 1974.

7. Subcritical Flutter Testing and System Identification, Houbolt, A.R.A.P.

Report No. 219, 1974.

8. Proceedings of the Flight Flutter Testing Symposium, May 1958, Washington, D.C., O.S.R.-9-0269.