Thermal stresses due to Disturbance of Uniform Heat Flow by an Insulated Hole of Aerofoil Cross Section

  • B.N. Sreenivas Rao Osmania University, Hyderabad
  • P. K. Potay Defence Metallurgical Research Laboratory, Hyderabad
DOI: https://doi.org/10.14429/dsj.17.7396
Keywords: Ovaloid, Elliptical, Aerofoil Cross Section

Abstract

The problems of thermal stresses for ovaloid and elliptical cross-sections have been solved by A.L. Florence, J.N. Goodier and G.C.Sih. In this paper the authors have generalised the results to determine the thermal stresses due to disturbance of uniform heat flow by an insulated hole of aerofoil cross section by making use of complex variable techniques.
Published
2014-05-21
How to Cite
Rao, B., & Potay, P. (2014). Thermal stresses due to Disturbance of Uniform Heat Flow by an Insulated Hole of Aerofoil Cross Section. Defence Science Journal, 17(4), 209-214. https://doi.org/10.14429/dsj.17.7396
Issue
Vol 17 No 4
Section
Research Papers
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