Modernization of the DISA 55D41 Wind Tunnel for Micro-Scale Probe Testing

Originally introduced in the 1960s by DISA Elektronik as a calibration tunnel for hot-wire anemometers, the Type 55D41 has now been reengineered into a versatile and modern aerodynamic test platform. While retaining key legacy components, such as the converging nozzle and the 55D42 power unit, the upgraded system features a redesigned modular test section with optical-grade quartz windows. This enhancement enables compatibility with advanced flow diagnostics and visualization methods, including PTV, DIC, and schlieren imaging. The modernized facility maintains the precision and flow stability that made the original design widely respected, while expanding its functionality to meet the demands of contemporary experimental research. Its architecture supports the aerodynamic characterization of micro-scale static pressure probes used in aerospace, propulsion, and micro gas turbine applications. Special attention is given to assessing the influence of probe tip geometry (e.g., conical, ogive), port positioning, and stem interference on measurement accuracy.

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Publication Details

Journal
Inventions
Published
2025-08-01
DOI
https://doi.org/10.3390/inventions10040066
Primary Topic
Fluid Dynamics and Turbulent Flows
Type
article
Field-Weighted Citation Impact
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article

Modernization of the DISA 55D41 Wind Tunnel for Micro-Scale Probe Testing

Oana Dumitrescu, Emilia Georgiana Prisăcariu, Iulian Vlăducă, Sergiu Strătilă et al.
Inventions
Fluid Dynamics and Turbulent Flows
article

Modernization of the DISA 55D41 Wind Tunnel for Micro-Scale Probe Testing

Oana Dumitrescu, Emilia Georgiana Prisăcariu, Iulian Vlăducă, Sergiu Strătilă, Raluca Andreea Roșu
article en

Abstract

Originally introduced in the 1960s by DISA Elektronik as a calibration tunnel for hot-wire anemometers, the Type 55D41 has now been reengineered into a versatile and modern aerodynamic test platform. While retaining key legacy components, such as the converging nozzle and the 55D42 power unit, the upgraded system features a redesigned modular test section with optical-grade quartz windows. This enhancement enables compatibility with advanced flow diagnostics and visualization methods, including PTV, DIC, and schlieren imaging. The modernized facility maintains the precision and flow stability that made the original design widely respected, while expanding its functionality to meet the demands of contemporary experimental research. Its architecture supports the aerodynamic characterization of micro-scale static pressure probes used in aerospace, propulsion, and micro gas turbine applications. Special attention is given to assessing the influence of probe tip geometry (e.g., conical, ogive), port positioning, and stem interference on measurement accuracy.

InventionsVol. 10(4)
Romanian Research and Development Institute for Gas Turbines (RO)
Openalex Percentile: Top 80%
Fluid Dynamics and Turbulent Flows
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