Two Dimensional Motion of an Oscillating Airfoil in a Fluctuating on Coming Stream at Supersonic Speed

  • J. P. Sharma Defence Science Laboratory, Delhi
DOI: https://doi.org/10.14429/dsj.25.6606
Keywords: Aerodynamics, Laplace Transformation

Abstract

The aerodynamic characteristics of a lifting body are studied for the case of a non uniform oncoming stream at supersonic speed past a thin oscillating airfoil at a small angle of attack. The two motions are assumed independent of each other and the coupled motion is analyzed using the theory of small disturbances. Analytic solution of the linearized problem is then obtained by applying Laplace transformation to it.
Published
2014-10-01
How to Cite
Sharma, J. (2014). Two Dimensional Motion of an Oscillating Airfoil in a Fluctuating on Coming Stream at Supersonic Speed. Defence Science Journal, 25(4), 133-138. https://doi.org/10.14429/dsj.25.6606
Issue
Vol 25 No 4
Section
Research Papers
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