Krishnamurthy, R and Sarma, BS and Deshpande, SM (2004) Kinetic scheme for computational aeroelastic analysis of 2-D airfoils in transonic flows. In: 34th AIAA Fluid Dynamics Conference and Exhibit 2004, 28 June through 1 July 2004, Portland, OR; United States.
|
PDF
AIAA_FLU_DYN_CON_EXH_2004.pdf - Published Version Download (339kB) | Preview |
Abstract
A new formulation based on a Kinetic scheme namely the Kinetic Flux Vector Splitting scheme on Moving Grids(KFMG) for solving Euler equations has been developed for unsteady flow computations around oscillating bodies. The necessary grid movement has been achieved using spring analogy method on structured grids. An integrated Aeroelastic code has been developed by coupling the KFMG Euler solver with a 2-DOF structural dynamics model of an airfoil. Results obtained for steady and unsteady flows problems are compared with literature data and are discussed in detail. The aeroelastic response characteristics for NACA 64A006 airfoil undergoing pitch and plunge motions have been obtained using the present aeroelastic code. The well known 'Transonic Dip' phenomenon has been captured for NACA 64A006 airfoil using the present Computational Aeroelastic code. © 2004 by the American Institute of Aeronautics and Astronautics, Inc.
Item Type: | Conference Paper |
---|---|
Publication: | 34th AIAA Fluid Dynamics Conference and Exhibit |
Publisher: | American Institute of Aeronautics and Astronautics Inc. |
Additional Information: | cited By 1; Conference of 34th AIAA Fluid Dynamics Conference and Exhibit 2004 ; Conference Date: 28 June 2004 Through 1 July 2004; Conference Code:102987 |
Keywords: | Airfoils; Codes (symbols); Kinetics; Oscillating flow; Structural dynamics; Transonic aerodynamics, Aeroelastic analysis; Aeroelastic response; Kinetic flux-vector splitting scheme; Literature data; Spring analogies; Structural dynamics models; Structured grid; Unsteady flow computations, Aeroelasticity |
Department/Centre: | Division of Mechanical Sciences > Aerospace Engineering(Formerly Aeronautical Engineering) |
Date Deposited: | 02 Dec 2020 11:41 |
Last Modified: | 02 Dec 2020 11:41 |
URI: | http://eprints.iisc.ac.in/id/eprint/66071 |
Actions (login required)
![]() |
View Item |