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keywords:(Two-phase flow)
Gravity Dependent Two-Phase Research at the NASA Glenn Research Center
Micro- and Nano-Scale Electrically Driven Two-Phase Thermal Management
Cryogenic Propellant Tank Self-Pressurization and Active Pressure Control
Cryogenic Propellant Tank Self-Pressurization and Active Pressure Control
Analysis of single- and two-phase flows in turbopump inducers.
Analysis of single- and two-phase flows in turbopump inducers.
Cryogenic propellant venting under low pressure conditions final report
Experimental Investigation of an Insector Device
Critical Flowrate of Two-Phase Nitrogen
Multiphase Flow Research on the International Space Station
Development of the Two Phase Flow Separator Experiment for a Reduced Gravity Aircraft Flight
Constitutive Relationships and Models in Continuum Theories of Multiphase Flows
Sensors and Components for Aerospace Thermal Control, Life Sciences and Propellant Systems
Sterilizable Liquid Propulsion System Quarterly Report, 1 Jan. - 31 Mar. 1969
Contained Liquid Experiments on Spacelab 1
A Preliminary Parametric Study of a Water-Augmented Air-Jet for High-Speed Ship Propulsion
Gravity Dependent Two-Phase Research at the NASA Glenn Research Center
Analytical Study of Liquid Metal Condensing inside Tubes
Analytical Study of Liquid Metal Condensing inside Tubes
Two-Phase Flow Technology Developed and Demonstrated for the Vision for Exploration
Two-Phase Heat Transport Systems for Spacecraft Scaling with Respect to Gravity
Pseudo-Sonic Velocity and Pseudo- Mach Number Concepts in Two-Phase Flows
NASA's Microgravity Fluid Physics Strategic Research Roadmap
Space Station Heat Pipe Advanced Radiator Element Prelaunch Mission Operation Report (SHARE)
Extension of the Physical Characteristics Program for Freon 12
Sensors and Components for Aerospace Thermal Control and Propellant Systems
RCM2 10 Bars Test Case. Combustion of Cryogenic Propellant at 10 Bars Using the CPS Code
Test Loops for Two-Phase Thermal Management System Components
In-Orbit Demonstration of Two-Phase Heat Transport Technology: TPX/G557 Flight Results
Spacecraft Thermal Control Design Data, Volume 4
Reference Design Study of Mist-Jet Propulsion Systems in Captured-Air-Bubble Ships
Modeling of Nonlinear Combustion Instability in Solid Propellant Rocket Motors
Effect of Variable Gravity on the Cooling Performance of a 16- Nozzle Spray Array