Publikationsdatum:
2019-06-28
Beschreibung:
The TranAir computer program calculates transonic flow about arbitrary configurations at subsonic, transonic, and supersonic freestream Mach numbers. TranAir solves the nonlinear full potential equations subject to a variety of boundary conditions modeling wakes, inlets, exhausts, porous walls, and impermeable surfaces. Regions with different total temperature and pressure can be represented. The user's manual describes how to run the TranAir program and its graphical support programs.
Schlagwort(e):
AERODYNAMICS
Materialart:
NASA-CR-4349
,
A-90092
,
NAS 1.26:4349
Format:
application/pdf
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