References

Aeroelasticity

NASA

Author Title Date Document
Benjamin D. Goldman, Robert E. Bartels, Robert T. Biedron and Robert C. Scott A Nonlinear Modal Aeroelastic Solver for FUN3D February 2016 NASA/TM-2016-219013
John W. Edwards and Carol D. Wieseman Flutter and Divergence Analysis using the Generalized Aeroelastic Analysis Method January 1, 2003 NASA Technical Report
vivek Mukhopadhyay An Interactive Software for Conceptual Wing Flutter anlaysis and Parametric Study August 1996 NASA TM 110276
E. Carson Yates, Jr., and Li-Chuan Chu Static Aeroelastic Effects on the Flutter of a Supercritical Wing March 1987 NASA TM 89132
Timothy H. Cox and Glenn B. Gilyard Ground Vibration Test Results for Drones for Aerodynamic and Structural Testing (DAST)/Aeroelastic Research Wing (ARW-1R) Aircraft January 1986 NASA-TM-85906
Robert M. Laurenson and J.I. McPherson Design Procedures for Flutter-Free Surface Panels March 1977 NASA-CR-2801

AIAA

Author Title Date Document
Charles L. Ruhlin, Frank J. Rouch Jr., Catherine Waters Transonic Flutter Model Study of a Supercritical Wing and Winglet August 1983 Journal of Aircraft Vol. 20 No. 8
Kumar G. Bhatia, K.S. Nagaraja, Charles L. Ruhlin Winglet Effects on the Flutter of a Twin-Engine Transport-Type Wing July 1985 Journal of Aircraft Vol. 22 No. 7

Miscellaneous

Author Title Date Document
Paulo C. Greco Jr. and Chuan-Tau E. Lan Frequency Domain Unsteady Transonic Aerodynamics for Flutter and Limit Cycle Oscillation Prediction December 2010 ABCM Special Issue Vol. XXXII, No. 5
Earl Dowell, Kenneth Hall, Robert Kielb, Deman Tang, and Jeffrey Thomas Nonlinear Aeroelasticity of Current and Future Aerospace Vehicles September 29, 2008 Presentation Slides
John K. Ramsey NASA Aeroelasticity Handbook Volume 2: Design Guides; Part 2 November 2006 NASA/TP -- 2006-212490/VOL2/PART2
Lynn C. Rogers Optimum Selection of Design Variable Increments to Improve Flutter Characteristics January 1970 Technical Memorandum 70-1-FDTE
H. Wittmeyer and H. Templeton Criteria for the Prevention of Flutter of Tab Systems 1956 R. M. No. 2825