Abstract

Intrusive probes are critical tools in supersonic wind tunnel testing, enabling direct measurement of flow properties such as pressure and heat flux. To support these measurements, a single-axis intrusive arm was designed and implemented in the Missouri S&T Supersonic Wind Tunnel. The system is designed to maintains precise probe positioning, while withstanding the aerodynamic loads, and preserving a dynamic seal between the test section and ambient environment. Its modular design accommodates a range of probe types for various research applications. This paper presents the design methodology, including structural, mechanical, and aerodynamic considerations, and details the integration process. System performance was validated through a series of tests using a total pressure probe, which confirmed stable Mach 3 flow across the test section and demonstrated the arm's ability to deliver accurate, repeatable measurements. The addition of the intrusive arm significantly enhances the facility's diagnostic capabilities, providing a robust platform for advanced supersonic flow studies.

Department(s)

Mechanical and Aerospace Engineering

Publication Status

Full Access

Comments

Department of Mechanical and Aerospace Engineering, West Virginia University, Grant None

Keywords and Phrases

Dynamic Seals; Factor of Safety; Finite Element Analysis; Flow Conditions; Freestream Mach Number; Heat Flux; Particle Image Velocimetry; Pressure Probes; Stagnation Temperature; Supersonic Wind Tunnels

International Standard Book Number (ISBN)

978-162410738-2

Document Type

Article - Conference proceedings

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 2025 American Institute of Aeronautics and Astronautics, All rights reserved.

Publication Date

01 Jan 2025

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