Linear pyrolysis of thermoplastics in chemically reactive environments
1965; American Institute of Aeronautics and Astronautics; Volume: 3; Issue: 2 Linguagem: Inglês
10.2514/3.2837
ISSN1533-385X
AutoresR.F. McAlevy, James G. Hansel,
Tópico(s)Engineering and Material Science Research
Resumo16 Duffy, R. E., A static pressure measurement technique for chemical kinetic studies, Proceedings of the First International Congress on Instrumentation in Aerospace Simulation Facilities, pp. 23-1-23-18 (September 1964). 17 Yoshikawa, K. K. and Katzen, E. D., Charts for air flow properties in equilibrium and frozen flows in hypervelocity nozzles, NASA TN-D-693 (April 1963), 18 Jorgensen, L. H. and Baum, G. M., ''Charts for equilibrium flow properties of air in hypervelocity nozzles, NASA TN-D1333 (September 1962). 19 Geiger, R., Nonequilibrium solution for reservoir conditions of 500 psia, 4000°K, L = 4.74 cm, private communications, General Electric Missile and Space Vehicle Div., Valley Forge, Pa. (August 1963). 20 Lordi, J., Nonequilibrium solution for reservoir conditions of 250 psia, 7000°K, L = 2.0 and 3.0 cm., private communications, Cornell Aeronautical Labs., Buffalo, N. Y. (October 1963). 21 Lobb, R. K., Experimental measurements of shock detachment distances on spheres fired in air at hypervelocities, Specialists' Meeting on the High Temperature Aspects of Hypersonic Flow, Brussels (April 3-6, 1962).
Referência(s)