Data were obtained for two phase and gaseous choked flow nitrogen in a long constant area duct of 16200 L/D with a diverging diffuser attached to the exit. Flow rate data were taken along five isotherms (reduced temperature of 0.81, 0.96, 1.06, 1.12, and 2.34) for reduced pressures to 3. The flow rate data were mapped in the usual manner using stagnation conditions at the inlet mixing chamber upstream of the entrance length. The results are predictable by a two phase homogeneous equilibrium choking flow model which includes wall friction. A simplified theory which in essence decouples the long tube region from the high acceleration choking region also appears to predict the data resonably well, but about 15 percent low
Choked flow analogy for very low quality two-phase flows - homogeneous flow and hydraulic jump theor...
Under certain conditions, inlets with a Borda type geometry were shown to exhibit sufficiently stron...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76407/1/AIAA-1991-3545-390.pd
Two-phase choked flow rate and pressure distribution data are reported for subcooled nitrogen flowin...
Data are presented for the two phase choked flow of three cryogenic fluids - nitrogen, methane, and ...
Mass limiting flow characteristics for a 55 L/D tube with a Borda type inlet were assessed over larg...
Data are presented for two-phase critical flow through nozzles. Test results from two converging-div...
Choked flow rates and axial pressure distributions were measured for subcooled nitrogen in a converg...
Mass flux measurements associated with chocked flows through four Borda type inlet geometries: circu...
In order to accelerate the deployment of capture and storage (CCS), engineers need experimentally va...
LOX and LN2 data for two-phase critical flow through nozzles were acquired with precision control. T...
The paper examines the topologic structure of all possible solutions which can exist in flows throug...
Data are presented of an experiment in which subcooled liquid nitrogen was discharged through a shar...
Flow rates and pressure thermal profiles for two phase choked flows of fluid nitrogen were studied t...
Experimental and analytical results are presented for choked flows of fluid nitrogen over a range of...
Choked flow analogy for very low quality two-phase flows - homogeneous flow and hydraulic jump theor...
Under certain conditions, inlets with a Borda type geometry were shown to exhibit sufficiently stron...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76407/1/AIAA-1991-3545-390.pd
Two-phase choked flow rate and pressure distribution data are reported for subcooled nitrogen flowin...
Data are presented for the two phase choked flow of three cryogenic fluids - nitrogen, methane, and ...
Mass limiting flow characteristics for a 55 L/D tube with a Borda type inlet were assessed over larg...
Data are presented for two-phase critical flow through nozzles. Test results from two converging-div...
Choked flow rates and axial pressure distributions were measured for subcooled nitrogen in a converg...
Mass flux measurements associated with chocked flows through four Borda type inlet geometries: circu...
In order to accelerate the deployment of capture and storage (CCS), engineers need experimentally va...
LOX and LN2 data for two-phase critical flow through nozzles were acquired with precision control. T...
The paper examines the topologic structure of all possible solutions which can exist in flows throug...
Data are presented of an experiment in which subcooled liquid nitrogen was discharged through a shar...
Flow rates and pressure thermal profiles for two phase choked flows of fluid nitrogen were studied t...
Experimental and analytical results are presented for choked flows of fluid nitrogen over a range of...
Choked flow analogy for very low quality two-phase flows - homogeneous flow and hydraulic jump theor...
Under certain conditions, inlets with a Borda type geometry were shown to exhibit sufficiently stron...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76407/1/AIAA-1991-3545-390.pd