A two-fluid model for missile exhaust trail expansion /
Christopher Sherman, A.W. Guess.

Description

Main Author

Sherman, Christopher

Related Names

Guess, Arnold W., 1929-, author.
Air Force Cambridge Research Laboratories (U.S.)
GCA Corporation

Language(s)

English

Published

Bedford, Massachusetts : Geophysics Research Directorate, Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1962.

Subjects

Rocket engines > Rocket engines / Exhaust emissions.
Condensation trails.
Guided missiles.

Summary

Contents: Derivation of two fluid equations; Discussion of the two fluid equations; The question of equilibrium, Asymptotic behavior of two-fluid equations for early and intermediate phases, Asymptotic behavior of the two-fluid equations for late phase, Conversion of two-fluid equations to a form suitable for machine calculations, Derivation of equations of mementum and energy from the Boltzmann equation, Derivation of collision frequency, mementum transfer, and energy transfer for a hard sphere model, Detail of derivation of energy transfer formula.

Note

"GCA Technical Report 62-12-A."
"1 June 1962."

Physical Description

36 pages : illustrations ; 28 cm

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