Add to ORKGThe marker-and-cell numerical technique was applied to the study of axisymmetric and two-dimensional flow of liquid in containers under low gravity conditions. The purpose of the study was to provide the capability for numerically simulating liquid propellant motion in partially filled containers during a docking maneuver in orbit. A computer program to provide this capability for axisymmetric and two-dimensional flow was completed and computations were made for a number of hypothetical flow conditions
Space shuttle propellant dynamics during ET/Orbiter separation in the RTLS (return to launch site) m...
A study was conducted to determine the influence of liquid propellants on the dynamic loads for spac...
Liquid propellant sloshing in tilted axisymmetric cylindrical tanks for space shuttle application
A test program was conducted involving forty-five drops of liquid propellant in instrumented tanks. ...
An experimental program was conducted to examine the liquid flow patterns that result from the axial...
Engineers handbook applicable in prediction of low gravity behavior of liquids in rocket propellant ...
Liquid propellant behavior at zero gravity - differential equations to predict kinetics of liquid an...
An experimental study of several models used to analyze the longitudinal dynamics of oscillations in...
A computer program called HOPI was developed to predict reorientation flow dynamics, wherein liquids...
Liquid propellant behavior under space flight conditions and predicting Apollo spacecraft liquid sta...
Dynamic behavior of liquids in moving containers with applications to propellants in space vehicle f...
Experimental data are presented for verifying the computer program for computing propellant oscillat...
Natural convection in a spherical container with cooling at the center was numerically simulated usi...
Dynamic interaction between structure and liquid propellants in space shuttle vehicle model
During the abort sequence, the ET and orbiter separate under aerodynamic loading, with propellant re...
Space shuttle propellant dynamics during ET/Orbiter separation in the RTLS (return to launch site) m...
A study was conducted to determine the influence of liquid propellants on the dynamic loads for spac...
Liquid propellant sloshing in tilted axisymmetric cylindrical tanks for space shuttle application
A test program was conducted involving forty-five drops of liquid propellant in instrumented tanks. ...
An experimental program was conducted to examine the liquid flow patterns that result from the axial...
Engineers handbook applicable in prediction of low gravity behavior of liquids in rocket propellant ...
Liquid propellant behavior at zero gravity - differential equations to predict kinetics of liquid an...
An experimental study of several models used to analyze the longitudinal dynamics of oscillations in...
A computer program called HOPI was developed to predict reorientation flow dynamics, wherein liquids...
Liquid propellant behavior under space flight conditions and predicting Apollo spacecraft liquid sta...
Dynamic behavior of liquids in moving containers with applications to propellants in space vehicle f...
Experimental data are presented for verifying the computer program for computing propellant oscillat...
Natural convection in a spherical container with cooling at the center was numerically simulated usi...
Dynamic interaction between structure and liquid propellants in space shuttle vehicle model
During the abort sequence, the ET and orbiter separate under aerodynamic loading, with propellant re...
Space shuttle propellant dynamics during ET/Orbiter separation in the RTLS (return to launch site) m...
A study was conducted to determine the influence of liquid propellants on the dynamic loads for spac...
Liquid propellant sloshing in tilted axisymmetric cylindrical tanks for space shuttle application