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Evaluation of the aerothermodynamic field produced by a pseudospheric body of mercury type at M = 22.6 flying in air in thermodynamic equilibrium
Annals of Geophysics
Tlie differential equations valid after tlie shock are firstgiven in curvilinear coordinates; the cbosen unknowns are the two velocitycomponents and the entropy and enthalpy. A function of entropy andenthalpy is then determined, by ineans of wliich ali the thermodynamicvariables of the fluir are " coherently " approximated. Later on, the densityand ali the otlier kinematic and thermodynamic variables are calculatedimmediately after the shock, taking the angle a as a parameter. The shapeof thedoi:10.4401/ag-5234 doaj:abd6f591bf914185b3047d842e54e836 fatcat:3gmh6qrumfayxezie3lmagivyy