Beckmann, Herbert K.2016-04-212016-04-211961Knight, James Roger. "Performance of plasma jets at sonic velocity." (1961) Master’s Thesis, Rice University. <a href="https://hdl.handle.net/1911/89198">https://hdl.handle.net/1911/89198</a>.https://hdl.handle.net/1911/89198An experimental program was carried out to investigate the flow properties of partly ionized monatomic gases in the converging section of a nozzle. Choked flow was maintained at the throat, and the stagnation pressure, mass flow rate, and thrust at the throat were measured. The thrust at the throat is essentially a function of the stagnation pressure. Deviations from the predicted values were interpreted as representing losses due to heat transfer, friction, and turbulence. The thrust data was compared with the values predicted by a one-dimensional isentropic flow theory for partly ionized gases expanding in thermal equilibrium. The theory, presented in terms of dimensionless flow parameters, was valid for any monatomic gas. Data obtained, when plotted in dimensionless form, showed the same deviation from the idealized relationships for both helium and argon.34 ppengCopyright is held by the author, unless otherwise indicated. Permission to reuse, publish, or reproduce the work beyond the bounds of fair use or other exemptions to copyright law must be obtained from the copyright holder.Performance of plasma jets at sonic velocityThesisRICE0235reformatted digitalThesis M.E. 1961 KNIGHT