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 |
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 |
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 |