The Fourier transform theory is applied to the analytical determination of the disturbance velocity potential and pressure acting on a two-dimensional plate, in order to reexamine those of previous analyses by other investigators. Simplified expressions of the generalized forces are presented for incompressible and nearly incompressible flows. As the Mach number tends to zero, the virtual mass induced by an oscillating fluid becomes infinitely large for a natural mode symmetric with respect to the midchord point. It is recommended to take into account a symmetric mode which changes no fluid volume contained in a control surface, when a coupled flutter oscillation at very low Mach numbers is analyzed. Incorrectness in the generalized forces of the previous analyses is pointed out by comparing with the present analysis.
Skip Nav Destination
Article navigation
December 1980
Research Papers
Reexamination of Unsteady Fluid Dynamic Forces on a Two-Dimensional Finite Plate at Small Mach Numbers
Y. Matsuzaki,
Y. Matsuzaki
National Aerospace Laboratory, Jindaiji, Chofu, Tokyo, Japan
Search for other works by this author on:
T. Ueda
T. Ueda
National Aerospace Laboratory, Jindaiji, Chofu, Tokyo, Japan
Search for other works by this author on:
Y. Matsuzaki
National Aerospace Laboratory, Jindaiji, Chofu, Tokyo, Japan
T. Ueda
National Aerospace Laboratory, Jindaiji, Chofu, Tokyo, Japan
J. Appl. Mech. Dec 1980, 47(4): 720-724 (5 pages)
Published Online: December 1, 1980
Article history
Received:
September 1, 1979
Revised:
April 1, 1980
Online:
July 21, 2009
Article
Article discussed|
View article
Connected Content
Citation
Matsuzaki, Y., and Ueda, T. (December 1, 1980). "Reexamination of Unsteady Fluid Dynamic Forces on a Two-Dimensional Finite Plate at Small Mach Numbers." ASME. J. Appl. Mech. December 1980; 47(4): 720–724. https://doi.org/10.1115/1.3153780
Download citation file:
Get Email Alerts
Cited By
Related Articles
Analysis of Friction-Saturated Flutter Vibrations With a Fully Coupled Frequency Domain Method
J. Eng. Gas Turbines Power (November,2020)
A Navier–Stokes Analysis of the Stall Flutter Characteristics of the Buffum Cascade
J. Turbomach (October,2000)
Effects of Shock Waves on Aerodynamic Instability of Annular Cascade Oscillation in a Transonic Flow
J. Turbomach (July,1989)
Closed-Form Representation of Beam Response to Moving Line Loads
J. Appl. Mech (March,2001)
Related Proceedings Papers
Related Chapters
A Simple Carburetor
Case Studies in Fluid Mechanics with Sensitivities to Governing Variables
Experimental Investigation of Ventilated Supercavitation Under Unsteady Conditions
Proceedings of the 10th International Symposium on Cavitation (CAV2018)
Antilock-Braking System Using Fuzzy Logic
International Conference on Mechanical and Electrical Technology, 3rd, (ICMET-China 2011), Volumes 1–3