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Tables and charts of equilibrium normal shock and shock tube solutions for pure co2 with velocities to 16 km/second
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Wilder, S. E. Miller II, C. G. |
| Copyright Year | 1974 |
| Description | Equilibrium thermodynamic and flow properties are presented in tabulated and graphical form for moving, standing, and reflected normal shock waves in pure CO2, representative of Mars and Venus atmospheres. Properties include pressure, temperature, density, enthalpy, speed of sound, entropy, molecular weight ratio, isentropic exponent, velocity and species mole fractions. Incident (moving) shock velocities are varied from 1 to 16 km/sec for a range of initial pressure of 5 Newtons per square meter to 500 kilo Newtons per square meter. The present results are applicable to shock tube flows, and to free-flight conditions for a blunt body at high velocities. Working charts illustrating idealized shock-tube performance with CO2 test gas and heated helium and hydrogen driver gases are also presented. |
| File Size | 13098459 |
| Page Count | 239 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740020649 |
| Archival Resource Key | ark:/13960/t3qv8988z |
| Language | English |
| Publisher Date | 1974-07-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics Planetary Atmospheres Shock Waves Carbon Dioxide Flow Characteristics Chemical Properties Thermodynamic Properties Physical Properties Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
