论文信息 - Hypersonic shock-heated flow parameters for velocities to 46,000 feet per second and altitudes to 323,000 feet - 字舞流文

Hypersonic shock-heated flow parameters for velocities to 46,000 feet per second and altitudes to 323,000 feet

[1] W. E. Moeckel,et al. Composition and thermodynamic properties of air in chemical equilibrium , 1958 .

[2] C. Wittliff,et al. NORMAL SHOCK WAVE PARAMETERS IN EQUILIBRIUM AIR , 1961 .

[3] H. W. Woolley,et al. TABLES OF THERMODYNAMIC PROPERTIES OF AIR INCLUDING DISSOCIATION AND IONIZATION FROM 1,500 K TO 15,000 K , 1959 .