Study of the effect of composition on the microstructure and thermophysical properties of niobium-based refractory systems


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详细

The structure and thermophysical properties—thermal diffusivity, thermal conductivity, linear thermal expansion coefficient, and specific heat capacity—in a temperature range of 20–1400°C are studied; DSC analysis of Nb–Si composites containing 12–18 and 14 at % Si, which are prepared by hybrid spark plasma sintering and hot pressing, respectively, is conducted. The effect of the composition and temperature on the structure and characteristics of thermophysical properties is estimated.

作者简介

N. Burkovskaya

All-Russian Scientific Research Institute of Aviation Materials

Email: murasheva_v_v@mail.ru
俄罗斯联邦, Moscow

N. Sevostyanov

All-Russian Scientific Research Institute of Aviation Materials

Email: murasheva_v_v@mail.ru
俄罗斯联邦, Moscow

V. Murasheva

All-Russian Scientific Research Institute of Aviation Materials

编辑信件的主要联系方式.
Email: murasheva_v_v@mail.ru
俄罗斯联邦, Moscow

Yu. Loshchinin

All-Russian Scientific Research Institute of Aviation Materials

Email: murasheva_v_v@mail.ru
俄罗斯联邦, Moscow

T. Shcheglova

All-Russian Scientific Research Institute of Aviation Materials

Email: murasheva_v_v@mail.ru
俄罗斯联邦, Moscow

S. Pakhomkin

All-Russian Scientific Research Institute of Aviation Materials

Email: murasheva_v_v@mail.ru
俄罗斯联邦, Moscow

M. Razmakhov

All-Russian Scientific Research Institute of Aviation Materials

Email: murasheva_v_v@mail.ru
俄罗斯联邦, Moscow

F. Karachevtsev

All-Russian Scientific Research Institute of Aviation Materials

Email: murasheva_v_v@mail.ru
俄罗斯联邦, Moscow

I. Efimochkin

All-Russian Scientific Research Institute of Aviation Materials

Email: murasheva_v_v@mail.ru
俄罗斯联邦, Moscow

B. Shchetanov

All-Russian Scientific Research Institute of Aviation Materials

Email: murasheva_v_v@mail.ru
俄罗斯联邦, Moscow


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