Facilities and Test Engineering
New Compressor Added to Glenn's 450-psig Combustion Air System
Two-Dimensional Bifurcated Inlet Variable Cowl Lip Test Completed in 10- by 10-Foot Supersonic Wind Tunnel
Reflective Focused Schlieren System Improved for Use in 10- by 10-Foot Supersonic Wind Tunnel
Engineering Design and Analysis
Ultrasonic Waves in Water Visualized With Schlieren Imaging
Mars Spark Source Prototype Developed
Reduced-Noise Gas Flow Design Guide Developed as a Noise-Control Design Tool for Meeting Glenn's Hearing Conservation and Community Noise Goals
New Web Server—the Java Version of
Tempest
—Produced
Last updated April 24, 2000, by Nancy.L.Obryan@nasa.gov
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