One dimensional compound compressible nozzle flow solution dependence on initial conditions and nozzle geometry, discussing applications to bypass turbojets and solid propellant motors
Generalized one-dimensional, compound compressible nozzle flow
1970-03-01
Sonstige
Keine Angabe
Englisch
Compound-compressible nozzle flow
AIAA | 1966
|Generalized one-dimensional, steady, compressible flow
AIAA | 1993
|Generalized One-Dimensional, Steady, Compressible Flow (TN)
Online Contents | 1993
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