Boundary conditions for adsorbing-emitting electrodes in contact with seeded, dense plasmas
Author:
Affiliation:
1. McDonnell Douglas Astronautics Company, Western Division, Santa Monica, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.5681
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1. Stagnation Point Langmuir Probe in a Shock Tube-Theory and Measurements
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