论文信息 - Axial and circumferential variations of hot- gas-side heat-transfer rates in a hydrogen- oxygen rocket - 字舞流文

Axial and circumferential variations of hot- gas-side heat-transfer rates in a hydrogen- oxygen rocket

Axial and circumferential variations of hot gas side heat transfer coefficients in hydrogen oxygen engines for use in nozzle and injector design

R. J. Quentmeyer | R. Schacht

[1] G. Kuznetsov,et al. Extinguishing a Ground Forest Fire by Spraying Water Over its Edge , 2018, Journal of Engineering Physics and Thermophysics.

[2] Von Glahn. Correlation of gas-side heat transfer for axisymmetric rocket engine nozzles , 1969 .

[3] W. L. Jones,et al. Experimental investigation of hot-gas side heat-transfer rates for a hydrogen-oxygen rocket , 1965 .

[4] Lloyd H. Back,et al. Convective heat transfer in a convergent-divergent nozzle , 1964 .

[5] Sanford Gordon,et al. A General IBM 704 or 7090 Computer Program for Computation of Chemical Equilibrium Compositions, Rocket Performance, and Chapman-jouguet Detonations , 1962 .

[6] J. C. Jaeger,et al. Conduction of Heat in Solids , 1952 .

[7] R. Svehla. Thermodynamic and Transport Properties for the Hydrogen-Oxygen System. NASA SP-3011 , 1964 .