0
Discussion

Discussion: “The Lure of the Mean Axes” (Meirovitch, L., and Tuzcu, I., ASME J. Appl. Mech., 74(3), pp. 497–504)

[+] Author and Article Information
David K. Schmidt

Professor Emeritus
Department of Mechanical and Aerospace Engineering,
University of Colorado,
Colorado Springs, CO 80918
e-mail: dschmidt@uccs.edu

Manuscript received June 1, 2015; final manuscript received September 8, 2015; published online October 1, 2015. Assoc. Editor: Alexander F. Vakakis.

J. Appl. Mech 82(12), 125501 (Oct 01, 2015) (5 pages) Paper No: JAM-15-1282; doi: 10.1115/1.4031567 History: Received June 01, 2015; Revised September 08, 2015

First Page Preview

View Large
First page PDF preview
FIGURES IN THIS ARTICLE
Copyright © 2015 by ASME
Your Session has timed out. Please sign back in to continue.

References

Meirovitch, L. , and Tuzcu, I. , 2007, “ The Lure of the Mean Axes,” ASME J. Appl. Mech., 74(3), pp. 497–504. [CrossRef]
Dusto, A. R. , Brune, G. W. , Dornfield, G. M. , Mercer, J. E. , Pilet, S. C. , Rubbert, P. E. , Schwanz, R. C. , Smutney, P. , Tinoco, E. N. , and Weber, J. A. , 1974, “ A Method for Predicting the Stability Characteristics of an Elastic Airplane,” Vol. 1-FLEXSTAB Theoretical Description, NASA Report No. CR-114712. (Ref. [5] in the subject article.)
Canavin, J. R. , and Likins, P. W. , 1977, “ Floating Reference Frames for Flexible Spacecraft,” AIAA J. Spacecr. Rockets, 14(12), pp. 724–732. (Ref. [4] in the subject article.)
Waszak, M. R. , and Schmidt, D. K. , 1988, “ Flight Dynamics of Aeroelastic Vehicles,” J. Aircr., 25(6), pp. 563–571. [CrossRef]
Buttrill, C. S. , Zeiler, T. A. , and Arbuckle, P. D. , 1987, “ Nonlinear Simulation of a Flexible Aircraft in Maneuvering Flight,” AIAA Paper No. 87-2501-CP.
Meirovitch, L. , 1967, Analytical Methods in Vibrations, Macmillan, New York.
Bisplinghoff, R. I. , and Ashley, H. , 1962, Principles of Aeroelasticity, Wiley, New York. (Ref. [1] in the subject article.)
Milne, R. D. , 1964, Dynamics of the Deformable Aeroplane, British Aeronautical Research Council, London, Reports and Memoranda No. 3395.
Cavin, R. K., III , and Dusto, A. R. , 1977, “ Hamilton's Principle: Finite Element Methods and Flexible Body Dynamics,” AIAA J., 15(12), pp. 1684–1690. [CrossRef]
Zeiler, T. A. , and Buttrill, C. S. , 1988, “ Dynamic Analysis of an Unrestrained, Rotating Structure Through Nonlinear Simulation,” AIAA Paper No. 88-2232-CP, April, 1988.
Buttrill, C. S. , 1988, “ Results of Including Geometric Non-Linearities in an Aeroelastic Model of an F/A-18,” NASA Conference Publication 3031, Recent Advances in Multidisciplinary Analysis and Optimization, Hampton, VA, Paper No. N89-25190.
Schmidt, D. K. , 2012, Modern Flight Dynamics, McGraw-Hill, New York.
Bryan, G. H. , and Williams, W. E. , 1904, “ The Longitudinal Stability of Gliders,” Proc. R. Soc., A, 73, pp. 100–116. [CrossRef]

Figures

Tables

Errata

Discussions

Related

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In