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Appendix 4 APPENDIX 4. ACKNOWLEDGMENTS, REFERENCES AND BIBLIOGRAPHY
ACKNOWLEDGMENTS
1. Acknowledgment is given to Mr. George S. Rasmussen, Structures DER, for his contribution in the development of the data presented in appendix 2 for whirl mode flutter analysis.
REFERENCES:
1. Airframe and Equipment Engineering Report No. 45, 99Simplified Flutter Prevention Criteria for Personal Type Aircraft." FAA, Engineering and Manufacturing Division, Flight Standards Service, Washington, D.C.
2. Introduction to the Study of Aircraft Vibration and Flutter, Scanlan and Rosenbaum, McMillan Company, New York, 1951.
3. Aeroelasticity, Bisplinghoff, Ashley, and Halfman, Addison-Wesley Publishing Co., Reading, Mass., 1955,
4. Application of Three-Dimensional Flutter Theory to Aircraft Structures, Air Force Technical Report (A.F.T.R.) 4798, 1942.
5. Tab Flutter Theory and Application, Air Force Technical Report, A.F.T.R., 5153, 1944.
6. The Use of Vectors in Vibration Measurement and Analysis, Kennedy and Pancu, Journal of Aeronautical Sciences, J.A.S., Vol. 14, 1947.
7. A Survey of Flight Flutter Testing Techniques, AGARD Flight Test Manual, Vol. 11, Chapter 14.
8. Mechanical Vibrations, Thomson, Prentice-Hall, New York, 1953.
9. An Analytical Treatment of Aircraft Propeller Precession Instability, Reed and Bland, NASA TN D-659.
10. Propeller Nacelle Whirl Flutter, Houbolt and Reed, Journal of Aeronautical Sciences (J.A.S.) March, 1962.
11. Review of Propeller-Rotor Whirl Flutter, NASA TR-264, July, 1967.
12. Cantilevered Power Package Whirl Mode Flutter Program, G.S. Rasmussen & Associates, Report No. 650, June 1, 1971.
13. Wind-Tunnel Measurement of Propeller Whirl-Flutter Speeds and Static Stability Derivatives and Comparison with Theory, NASA TN D-1807, August 1963.
14. Laguerre's Method Applied to the Matrix Eigenvalue Problem Beresford Parlett, A Paper Prepared Under Contract AT (30-l)-1480 with the U.S.A.E.C.
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.