Publikationsdatum:
2019-06-27
Beschreibung:
The viscous-shock-layer equations for hypersonic laminar and turbulent flows of radiating or nonradiating gas mixtures in chemical equilibrium are presented for two-dimensional and axially-symmetric flow fields. Solutions were obtained using an implicit finite-difference scheme and results are presented for hypersonic flow over spherically-blunted cone configurations at freestream conditions representative of entry into the atmosphere of Venus. These data are compared with solutions obtained using other methods of analysis.
Schlagwort(e):
FLUID MECHANICS AND HEAT TRANSFER
Materialart:
NASA-CR-143204
,
TR-75-T9
Format:
application/pdf
