A method for quickly solving a pressure conduction delay correction parameter of a wind tunnel test
By optimizing the scanning valve layout and data processing methods in wind tunnel tests, the problems of large computational load and poor timeliness in pressure transmission delay synchronization processing were solved, achieving fast and accurate pressure data synchronization correction and meeting the real-time analysis requirements of aircraft model tests.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- INST OF HIGH SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENT
- Filing Date
- 2023-06-12
- Publication Date
- 2026-07-21
AI Technical Summary
In existing technologies, the synchronous processing of pressure transmission delay in continuous variable angle of attack pressure measurement tests in wind tunnels involves large computational loads, is cumbersome to operate, and has poor timeliness, failing to meet the need for rapid acquisition of detailed and accurate test data.
In a stepped pressure test, scanning valve modules were set up inside the model cavity with consistent pipe lengths. High-frequency sampling was used to acquire data, and suitable measurement points were selected using interpolation, linear fitting, and graphical display tools. Combined with pre-correction parameters and linear or quadratic fitting, pressure transmission delay correction parameters were quickly calculated.
It significantly reduces the amount and complexity of computational data, quickly obtains synchronous correction parameters, improves the accuracy and timeliness of data processing, and meets the real-time analysis requirements of wind tunnel tests.
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Figure CN117168753B_ABST