|
Related articles:
Aerodynamics
Mach number
Supersonic
Scramjet
Transonic
Reaction Engines A2
Rocket engine
Space Shuttle
Atmospheric reentry
Key terms: gas flow regime shock effects km speeds around mach number increase temperature become energy gases mean similarity border change modeling above ionization supersonic lower allow hypersonic flows dissociation pressure begins generally important equations surface entropy perfect viscous subsonic chemical boundary layer variables radiation optically stagnation shock wave separately around mach aerodynamics reaction engines hypersonic regime effect on the flow similarity parameters Search external links cited by footnotes on Wikipedia page Hypersonic: |
|