D19 (1190)
For the power elements of the structures of aircraft, car bodies, pipes, etc., operating at temperatures up to 200−250 degrees.
For the power elements of the structures of aircraft, car bodies, pipes, etc., operating at temperatures up to 200−250 degrees.
| Standard | Fe, % | Si, % | Be, % | Mg, % | Mn, % | Ti, % | Cu, % | Zn, % | Al, % |
|---|---|---|---|---|---|---|---|---|---|
| Standard | Fe, % | Si, % | Be, % | Mg, % | Mn, % | Ti, % | Cu, % | Zn, % | Al, % |
| GOST 4784-97 | < 0.5 | < 0.5 | 0.0002–0.005 | 1.7–2.3 | 0.5–1 | < 0.1 | 3.8–4.3 | < 0.1 | 91.095–94 |
| Temperature, °C | E\cdot 10^{9}, MPa | \alpha\cdot 10^{6}, K^{-1} | \varkappa, \frac{W}{m\cdot K} | \rho, \frac{kg}{m^3} | c\cdot 10^{-3}, \frac{J}{kg\cdot K} | R\cdot 10^{-6}, \Omega\cdot m |
|---|---|---|---|---|---|---|
| Temperature, °C | E\cdot 10^{9}, MPa | \alpha\cdot 10^{6}, K^{-1} | \varkappa, \frac{W}{m\cdot K} | \rho, \frac{kg}{m^3} | c\cdot 10^{-3}, \frac{J}{kg\cdot K} | R\cdot 10^{-6}, \Omega\cdot m |
| 20 | 70 | 2760 | 0.061 | |||
| 100 | 20.3 | 138 | 0.88 |
| Standard | Description |
|---|---|
| Standard | Description |
| GOST 4784-97 |
| Parameter | Units of measurement | Description |
|---|---|---|
| Parameter | Units of measurement | Description |
| E\cdot 10^{9} | MPa | Elastic modulus |
| \alpha\cdot 10^{6} | K^{-1} | Coefficient of thermal (linear) expansion (range 20°C–T) |
| \varkappa | \frac{W}{m\cdot K} | Coefficient of thermal conductivity (the heat capacity of the material) |
| \rho | \frac{kg}{m^3} | The density of the material |
| c\cdot 10^{-3} | \frac{J}{kg\cdot K} | The specific heat of the material (range 20°C–T) |
| R\cdot 10^{-6} | \Omega\cdot m | Electrical resistivity |