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Influence of Actuator Movement Rate During Acquisition of Inlet Characterization DataThis report considers using a process to acquire performance data for supersonic mixed-compression inlets that is faster and less costly than the previous process. In the previous process for acquiring data during wind tunnel experiments, actuators for backpressuring an inlet moved in discrete increments, paused for dynamics to dampen, measured data for 5 s, recorded the data, and then reduced the data to graphic plots of pressure recovery versus mass capture ratio. This discrete data acquisition procedure was methodical, reliable, and accurate. However, acquiring data to characterize the inlet consumed significant wind-on time. Wind tunnel operation was costly when considering maintenance, energy, and human resources (operators and research team); therefore, the price for each data point was high. This report presents a quicker method to obtain all measurements, one which can also be used in blowdown wind tunnels. This approach, identified as the dynamic inlet characteristic data acquisition procedure, uses in situ dynamic high-speed pressure sensors to measure pressure signals. The backpressuring actuator moves continuously, and measurements from high-speed pressure sensors are recorded as the actuator progresses to and past the incremental points. Despite its advantages, the approach raised the following questions: (1) Will the new process be as accurate as the previous process? and (2) Are there any hidden costs? These concerns are addressed in this report. This report reviews a study that was undertaken to compare wind tunnel experiment data taken using the previous discrete data acquisition procedure with data recorded using the dynamic inlet characterization data acquisition procedure. In this report, the wind tunnel experiment and the study objectives are described. The processes to reduce the data for analysis are explained, and a discussion of the results is given. Finally, conclusions from this study that may guide further work in this area are presented.
Document ID
20240013421
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
T Shane Sowers
(HX5, LLC)
Thomas J Stueber
(Glenn Research Center Cleveland, United States)
Date Acquired
October 22, 2024
Publication Date
January 1, 2025
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Research and Support Facilities (Air)
Instrumentation and Photography
Report/Patent Number
E-20277
NASA/TM-20240013421
Funding Number(s)
WBS: 725017.02.03.02.03.07
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Inlet Characterization Curves
Actuator Movement
Inlets
Wind Tunnel Experiements
Instrumentation
Data Acquisition
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