Zobrazeno 1 - 10
of 79
pro vyhledávání: '"I. N. Fridlyander"'
Autor:
I. N. Fridlyander
Publikováno v:
Herald of the Russian Academy of Sciences. 78:416-420
Publikováno v:
Metal Science and Heat Treatment. 49:279-283
Mechanical properties under static and dynamic loads, fatigue characteristics, fracture toughness, high-temperature strength, corrosion resistance, and physical and thermophysical properties of pressed alloy V-1469 in state T1 are studied. The alloy
Autor:
I. N. Fridlyander
Publikováno v:
Metal Science and Heat Treatment. 45:337-340
Autor:
I. N. Fridlyander
Publikováno v:
Metal Science and Heat Treatment. 45:344-347
Autor:
G. M. Goloviznina, I. N. Fridlyander, V. V. Berstenev, L. P. Lantsova, E. A. Tkachenko, L. V. Latushkina
Publikováno v:
Metal Science and Heat Treatment. 45:239-245
Mechanical properties and the grain size of alloy D16ch and 1163 used for the sheeting of aircraft fuselages after 21% and 74% deformation and different kinds of heat treatment are studied. The effect of the modes of intermediate, preliminary, and fi
Autor:
I. N. Fridlyander, G.V. Cherepok, V.A. Grinevich, E. A. Tkachenko, L. V. Latushkina, V. V. Berstenev, I.P. Zhegina
Publikováno v:
Materials Science Forum. :1347-1352
Autor:
I. N. Fridlyander
Publikováno v:
Metal Science and Heat Treatment. 44:292-296
Aluminum and magnesium alloys are the base structural materials in aircraft and spacecraft engineering. The main stages of the development and introduction of light alloys are described.
Publikováno v:
Metal Science and Heat Treatment. 43:298-301
A comprehensive study of the suitability of sheets of alloy 1441 of the Al – Cu – Mg – Li system for the production of long-life airplane fuselages is described. The alloy has been used in the Be 103 boatplane airframe and is tested for use in
Autor:
I. N. Fridlyander
Publikováno v:
Metal Science and Heat Treatment. 43:6-10
Publikováno v:
High Temperature. 39:507-510
The Knudsen effusion method with mass-spectrometric analysis of evaporation products is used to determine the composition and pressure of saturated vapor over liquid lithium in the temperature range from 627 to 893 K. The Li(l) = Li(g), 2Li(l) = Li2(