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Fluids
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Intense Convection That is Problematic for GPROF, XCAL, and Precipitation Features
Settled Cryogenic Propellant Transfer
Centaur Test Bed (CTB) for Cryogenic Fluid Management
Propulsion: Launch, In-Space Related Ground Technologies
Flight Development for Cryogenic Fluid Management in Support of Exploration Missions
Shuttle Return To Flight Experimental Results: Cavity Effects on Boundary Layer Transition
Amphibious Vehicle Water Egress Modeling and Simulation Using CFD and Wong's Methodology
Wind-US Unstructured Flow Solutions for a Transonic Diffuser
Optically Based Flame Detection in the NASA Langley 8-ft High- Temperature Wind Tunnel
SLS Dual Use Upper Stage (DUUS) Opportunities
Preliminary Results from Propellant Mass Gauging with Electrical Capacitance Tomography
Hover and Forward Flight Performance Modeling of the Ingenuity Mars Helicopter
Transonic flow in a converging-diverging nozzle Final report
Advanced feed system component interaction analysis Quarterly status letter, 30 Jun. - 30 Sep. 1969
Survey of Solver-Related Geometry and Meshing Issues
Cryogenic Fluid Management: 2000-2004
Farfield structure of an aircraft trailing vortex, including effects of mass injection
Propellant dynamic problems in space shuttle vehicles, part 2 Final report
The hydraulic characteristics of flow through miniature slot orifices
Low Gravity Issues of Deep Space Refueling
Nearfield Anisotropic Mesh Adaptation for the Third AIAA Sonic Boom Workshop
A two spacecraft test of a single spacecraft method of estimating shock normals
Experimental investigation of containment in constant-temperature radial-inflow vortexes
Study of the accuracy of gas flow measurements using the sonic throat method
Single stage experimental evaluation of compressor blading with slots and wall flow fences
Evaluation of Navy 9 cst Oil in Bell Helicopter M412 HP Gearboxes
Hypersonic shock-interaction phenomena applicable to space shuttle configurations
Transonic flow in a converging-diverging nozzle Final report
Investigation of the steady expansion of a gaseous axisymmetric jet into a vacuum Final report
Diffusion of trace gases for leak detection in aerospace systems