论文信息 - Flight test analysis of Apollo heat shield material using the Pacemaker vehicle system - 字舞流文

Flight test analysis of Apollo heat shield material using the Pacemaker vehicle system

Ablation and temperature data for Apollo heat shield material using Pacemaker vehicle for flight test

R. A. Graves | W. G. Witte | W. Witte

[1] J. C. Dunavant,et al. Effect of roughness on heat transfer to hemisphere cylinders at Mach numbers 10.4 and 11.4 , 1967 .

[2] E. Zoby,et al. Correlation of free-flight turbulent heat-transfer data from axisymmetric bodies with compressible flat-plate relationships , 1967 .

[3] W. A. Brooks,et al. Flight and ground tests of Apollo heat shield material , 1965 .

[4] Allan P. Colburn,et al. A method of correlating forced convection heat-transfer data and a comparison with fluid friction☆☆☆ , 1964 .

[5] C. Frederick Hansen,et al. Approximations for the thermodynamic and transport properties of high-temperature air , 1958 .

[6] L. Lees. Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight Speeds , 1956 .