Entrance heat transfer from a plasma stream in a circular tube - Engineering correlations.
Nusselt numbers correlated for entrance section heat transfer from helium, argon and nitrogen plasma jets in circular tubes
Choksi, N. M.↗
Engineering topics
Johnson, J. R.
Publications and source records attributed to Johnson, J. R..
Elimination of rocket engine asymmetric loads during tests at sea level
Secondary injection concept eliminates asymmetric loads and may increase thrust rocket engine loads during sea level tests. The concept uses either a tubular manifold with evenly spaced injection ports or secondary fluid injected at the turbine exhaust inlet to the thrust chamber.
Johnson, J. R.↗
Radial heat transfer from a plasma stream
Radial heat transfer from helium, argon, and nitrogen plasma streams
HEAT TRANSFER↗
Heat transfer from plasma jets space technology project no. 3
Explore the source record for details and available documents.
Eubank, P. T.↗