Nozzle characteristics in the transition regime between continuum and free molecular flow-Reference-Cited by-同舟云学术

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

Published:1964-06 Issue:6 Volume:2 Page:1088-1092
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

MILLIGAN MANCIL W.¹

Affiliation:

1. University of Tennessee, Knoxville, Tenn

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.2498

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

Cited by 24 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Design and numerical investigation to visualize the fluid flow and thermal characteristics of non-axisymmetric convergent nozzle;Engineering Science and Technology, an International Journal;2019-02

2. Study of the effects of preheated wall/plates in microthruster systems;Journal of Theoretical and Applied Mechanics;2018-07-20

3. Performance analysis of microelectromechanical thrusters using a direct simulation Monte Carlo solver;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2017-02-09

4. Numerical simulation of micro-nozzle and micro-nozzle-array flowfield characteristics;Vacuum;2008-09

5. Characteristics of micronozzle gas flows;Physics of Fluids;2007-03