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

Authors

  • 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.

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Published

2014-05-21

How to Cite

Rao, B. S., & Potay, P. K. (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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