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THERMAL STRESSES IN CIRCULAR DISCS.
National Aeronautics and Space Administration (NASA)

THERMAL STRESSES IN CIRCULAR DISCS.

Aerospace & Aviation Published 2019 Verification Pending

Overview & Synopsis

Analyses are presented for the elastic buckling of a thin circular disc subjected to a steady-state, two-dimensional, radially- symmetrical temperature gradient. Ritz minimizing procedure were used to evaluate parameters for the critical temperature difference and for the mode of buckling. Numerical solutions were obtained on a digital computer for the boundary conditions of inner radius fixed and outer radius either free or fixed for discs with diameter ratios of 1.25 to 12. values for the range of diameter ratios tested.

Indexed from repository: NASA Technical Reports Server (ntrs.nasa.gov)

Document Information

Document Title THERMAL STRESSES IN CIRCULAR DISCS.
Author / Organization National Aeronautics and Space Administration (NASA)
Subject & Discipline OTHER
Categories Aerospace & Aviation
Publication Year 2019
License / Rights Public Domain / NASA STI Open Access
Resource Verification Listed PDF (Verification Pending)
Original Host Website NASA Technical Reports Server (ntrs.nasa.gov)
File Format application/pdf (Portable Document Format)
Language EN
Catalog ID DOC-67178
Original Source Link Visit Source Page on ntrs.nasa.gov »