Nozzle characteristics in the transition regime between continuum and free molecular flow

Author:

MILLIGAN MANCIL W.1

Affiliation:

1. University of Tennessee, Knoxville, Tenn

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference3 articles.

1. Smetana, F O , "A. semiempirical desciiption of the discharge characteristics of the converging seel ion of a low-density hypersonic nozzle/7J Aerospace Sci 28, 988-989 (1961)

2. Folsom R G , Nozzle characteristics in high vacuum flowsrarefied gas dynamics ' Trans Am Soc Mech Engrs 74, 915-918(1952)

3. Gaskinetics and gasdynamics of orifice flow

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