Instrumentation and Control Technology
High Gas Temperature Probe
Thermal Analysis Demonstrated for a
Plug-Type Heat Flux Gauge
Reliable Breakdown Obtained in Silicon
Carbide Rectifiers
Ultraviolet Molecular Rayleigh
Scattering Used to Measure Velocity in High-Speed Flow
Chaotic Time Series Analysis Method
Developed for Stall Precursor Identification in High-Speed Compressors
Controls/CFD Interdisciplinary Research
Software Generates Low-Order Linear Models for Control Design From
Steady-State CFD Results
Single-Lever Power Control for General
Aviation Aircraft Promises Improved Efficiency and Simplified Pilot
Controls
Internal Fluid Mechanics
National Combustion Code: A Multidisciplinary
Combustor Design System
Interactive Educational Tool for Turbofan and
Afterburning Turbojet Engines
Rotor-Stator Interaction Performance Effects
Stator Indexing in Multistage Compressors
Bleed Hole Flow Phenomena Studied
Internal Mixing Studied for GE/ARL Ejector Nozzle
Propulsion Systems
High-Pressure Combustion Testing
Reveals Promise of Low-Emission Combustors for Advanced Subsonic
Gas Turbines
Computational Fluid Dynamics Analysis
Method Developed for Rocket-Based Combined Cycle Engine Inlet
Fluidic Injection for Throat-Area Control
and Thrust Vectoring
Oscillating Cascade Aerodynamics at Large
Mean Incidence Angles
SWIFT: Multistage Turbomachinery Analysis
Code Developed
Effects of Rotor Wake on Film Cooling
Investigated
Forward Swept Compressor Testing
Low Pressure Turbine Flow Physics Program
Vacuum Cleaner Fan Being Improved
Acoustic Barrier Facilitates Inlet Noise Measurements
for Aft-Dominated Fans
Aeropropulsion Facilities and Experiments
Scale Model Icing Research Tunnel
Supersonic Wind Tunnel Capabilities Expanded
Into Subsonic Region
Interdisciplinary Technology Office
pV3-Gold Visualization Environment for Computer
Simulations
Steady-State Cycle Deck Launcher Developed
for Numerical Propulsion System Simulation
Configuration Management File Manager
Developed for Numerical Propulsion System Simulation
Portable Extensible Viewer
Visual Computing Environment
A Vision in Aeronautics--The K-12 Wind Tunnel
Project
Flow Analysis of a Gas Turbine Low-Pressure
Subsystem
Last updated May 1, 1997
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