摘要: |
An abbreviated program was conducted in the NASA Lewis Research Center 8- by 6-Foot Supersonic Wind Tunnel to calibrate the test section and survey the flow quality following the installation of flow quality improvements in the facility. This program was designed to accommodate the specific requirements of an aeropropulsion research test program that took place before a complete test section calibration was conducted. Therefore, the flow quality goals for the 8- by 6-ft test section were based on the specific requirements of the research program and the facility's operational constraints. Test results indicate that flow quality in the test section was good and met or exceeded the agreed-upon goals at all except the Mach 2 setting. |