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Fluids
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Electrostatic Discharge (ESD) of Aerospace Vehicles
Initial Disturbance Fields For Boundary Layer Transition In Aerospace
Evaluation of Full Reynolds Stress Turbulence Models in FUN3D
Adjoint-Based Methodology for Time-Dependent Optimal Control (AMTOC)
Aero-Thermal Calibration of the NASA Glenn Icing Research Tunnel (2004 and 2005 Tests)
CFL3D Contribution to the AIAA Supersonic Shock Boundary Layer Interaction Workshop
Orion Active Thermal Control System Dynamic Modeling Using Simulink/MATLAB
Unsteady Full Annulus Simulations of a Transonic Axial Compressor Stage
Cryogenic Fluid Storage Technology Development: Recent and Planned Efforts at NASA
Cryogenic Orbital Testbed (CRYOTE) Ground Test Article, Final Report
Comparison Between Simulated and Experimentally Measured Performance of a Four Port Wave Rotor
Flutter Analysis of the Shuttle Tile Overlay Repair Concept
Reentry Thermal Analysis of a Generic Crew Exploration Vehicle Structure
Wall Boundary Layer Measurements for the NASA Langley Transonic Dynamics Tunnel
The Role of Flight Experiments in the Development of Cryogenic Fluid Management Technologies
Flight Development for Cryogenic Fluid Management in Support of Exploration Missions
Shuttle Return To Flight Experimental Results: Cavity Effects on Boundary Layer Transition
Settled Cryogenic Propellant Transfer
Centaur Test Bed (CTB) for Cryogenic Fluid Management
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
Wind-US Unstructured Flow Solutions for a Transonic Diffuser
Optically Based Flame Detection in the NASA Langley 8-ft High- Temperature Wind Tunnel
Low Gravity Issues of Deep Space Refueling
Transonic flow in a converging-diverging nozzle Final report
Advanced feed system component interaction analysis Quarterly status letter, 30 Jun. - 30 Sep. 1969
Characteristics of Separated Flow Regions Within Altitude Compensating Nozzles Final Report
A calibration and diagnosis of the test stream of an electric arc-heated wind tunnel
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
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