Wind Tunnel Experiment Of Aeroelastic Flutter
In this work, flutter behaviour of NACA 6409 is investigated using wind tunnel. The plunging and pitching oscillation of the wing is being observed to determine the dynamic instability point. The elastic axis will be manipulated in the experiment where the position of the elastic axis was varied at...
Main Author: | Mah, Chuen Tak |
---|---|
Format: | Monograph |
Language: | English |
Published: |
Universiti Sains Malaysia
2018
|
Subjects: | |
Online Access: | http://eprints.usm.my/52682/1/Wind%20Tunnel%20Experiment%20Of%20Aeroelastic%20Flutter_Mah%20Chuen%20Tak_A2_2018_MJMS.pdf |
Similar Items
-
Design and Development of an Experimental Aeroelastic Test Rig
by: Mohd. Rafie, A. S., et al.
Published: (2006) -
Design, construction, and testing of an open-loop low-speed wind tunnel
by: Muhammad Adnin, Mat Bahari
Published: (2012) -
Development Of The USM Wind Tunnel Validation Model For Calibration
by: Sim, Chiow Moon
Published: (2018) -
Structural Optimization of an Aeroelastically Tailored Composite Flat Plate Made of Woven Fiberglass/Epoxy
by: Attaran, A., et al.
Published: (2006) -
A study of drag force on different type of airfoil in a subsonic wind tunnel
by: Muhamad Faruqi, Zahari
Published: (2013)