Coupled Thermo-Structural Analysis Model of Solid Rocket Motor Nozzle considering the Variation of Friction Coefficient under Operating Conditions

Table 2

Material properties of carbon-phenolic-resin.

ρ	1430
T(°C)	E		v	G		T(K)	α(×10^−6)		T(K)	K		c
	X	Y/Z		XY/XZ	YZ		X	Y/Z		X	Y/Z	T	—
23	16.55	17.93	0.32	5.17	6.	366	16.67	13.33	273	0.8	1.08	273	880
93	12.41	17.24	0.29	4.83	6.55	477	22.1	8.84	473	0.93	1.5	373	1165
204	5.52	13.1	0.23	2.76	3.24	588	23.97	6.85	548	1	1.55	473	1450
315	1.38	8.96	0.13	1.03	2.21	699	24.81	4.96	1100	1	1.55	573	1475
426	0.55	6.9	0.08	1.03	1.86	810	25.29	1.95	1500	1.6	2.59	673	1500
537	0.34	6.55	0.06	1.1	1.72	1088	15.15	0	1900	1.6	3	1073	1500
815	0.34	7.58	0.05	1.38	1.79	1366	−5.7	0
1093	0.34	8.27	0.06	1.52	1.93	1911	−12.9	1.54
1648	0.34	6.9	0.07	1.52	2.07	2477	−13.8	8.02
2204	0.34	2.76	0.08	1.24	1.52	3033	−21.9	10.23
2760	0.34	1.38	0.09	0.48	0.69