Publikationsdatum:
2019-06-28
Beschreibung:
The PARC2D code has been selected to analyze the flowfields of a representative hypersonic scramjet nozzle over a range of flight conditions from Mach 3 to 20. The flowfields, wall pressures, wall skin friction values, heat transfer values and overall nozzle performance are presented.
Schlagwort(e):
AIRCRAFT PROPULSION AND POWER
Materialart:
NASA-CR-182150
,
E-4190
,
NAS 1.26:182150
Format:
application/pdf
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