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| Author | : Maynard C. Sandford |
| Publisher | : |
| Total Pages | : 65 |
| Release | : 1975 |
| Genre | : Airplanes |
| ISBN | : |
| Author | : Maynard C. Sandford |
| Publisher | : |
| Total Pages | : 76 |
| Release | : 1975 |
| Genre | : Airplanes |
| ISBN | : |
The application of active control technology to suppress flutter has been demonstrated successfully in the Langley transonic dynamics tunnel with a delta-wing model. The model was a simplified version of a proposed supersonic transport wing design. An active flutter-suppression method based on an aerodynamic energy criterion has been verified by using three different control laws. The first two control laws utilized both leading-edge and trailing-edge active control surfaces, whereas the third control law required only a single trailing-edge active control surface. At a Mach number of 0.9 the experimental results demonstrated increases in the flutter dynamic pressure from 12.5 percent to 30 percent with active controls. Analytical methods were developed to predict both open-loop and closed-loop stability, and the results agreed reasonably well with the experimental results.
| Author | : Maynard C. Sandford |
| Publisher | : |
| Total Pages | : 65 |
| Release | : 1975 |
| Genre | : Airplanes |
| ISBN | : |
| Author | : Maynard C. Sandford |
| Publisher | : |
| Total Pages | : 76 |
| Release | : 1975 |
| Genre | : Airplanes |
| ISBN | : |
| Author | : H. Honlinger |
| Publisher | : |
| Total Pages | : 91 |
| Release | : 1982 |
| Genre | : |
| ISBN | : |
Extensive research programs have been conducted at MBB and at AFWAL to investigate the application of active controls for the suppression of wing/store flutter. A flutter suppression system was developed and flight tested on an F-4F aircraft. The control law was designed by MBB using optimal control theory to minimize the control surface motion and to provide the required stability margins. During the test it was found that the dynamic behavior of the wing-pylon-store changed considerably with excitation amplitude due to free play and preload. The active flutter suppression system worked well and provided an increase in flutter speed. (Author).
| Author | : H. Hoenlinger |
| Publisher | : |
| Total Pages | : 66 |
| Release | : 1983 |
| Genre | : |
| ISBN | : |
A flutter suppression system was developed and flight tested on an F-4F aircraft. The control law was designed by MBB (Messerschmitt-Bolkow-Blohm GmbH) using optimal control theory to minimize the control surface motion and to provide the required stability margins. During the test it was found that the dynamic behavior of the wing-pylon-store changed considerably with excitation amplitude due to free play and preload. The active flutter suppression system worked well and provided an increase in flutter speed.
| Author | : |
| Publisher | : |
| Total Pages | : 79 |
| Release | : 2000* |
| Genre | : Flutter (Aerodynamics) |
| ISBN | : |
Extensive research programs have been conducted at Messerschmitt-Bolkow-Blohm GmbH (MBB) and at AFWAL to investigate the application of active controls for the suppression of wing/store flutter. A flutter suppression system was developed by MBB using optimal control theory to minimize the control surface motion and to provide the required stability margins. During the test it was found that the dynamic behavior of the wing-pylon-store changed considerably with excitation amplitude due to free play and preload. The active flutter suppression system worked well and provided an increase in flutter speed.
| Author | : Gregory S. Mason |
| Publisher | : |
| Total Pages | : 58 |
| Release | : 2002 |
| Genre | : |
| ISBN | : |
| Author | : National Aeronautics and Space Administration (NASA) |
| Publisher | : Createspace Independent Publishing Platform |
| Total Pages | : 48 |
| Release | : 2018-06-03 |
| Genre | : |
| ISBN | : 9781720631729 |
To study the effectiveness of various control system design methodologies, the NASA Langley Research Center initiated the Benchmark Active Controls Project. In this project, the various methodologies were applied to design a flutter suppression system for the Benchmark Active Controls Technology (BACT) Wing. This report describes the user's manual and software toolbox developed at the University of Washington to design a multirate flutter suppression control law for the BACT wing.Mason, Gregory S. and Berg, Martin C. and Mukhopadhyay, VivekLangley Research CenterWINGS; CONTROL SYSTEMS DESIGN; ACTIVE CONTROL; VIBRATION DAMPING; CONTROL THEORY; SYSTEMS ENGINEERING; USER MANUALS (COMPUTER PROGRAMS)
| Author | : Jennifer Heeg |
| Publisher | : |
| Total Pages | : 52 |
| Release | : 1993 |
| Genre | : Flutter (Aerodynamics) |
| ISBN | : |
