Abstract

The conventional pitot-static tube’s accuracy in measuring indicated airspeed is compromised by its longitudinal inclination during forward flight, causing errors when the angle surpasses a critical threshold. This study aimed to propose and assess new designs for pitot-static tube ports to mitigate the angle of attack. Modifications, such as enlarging the inlet cross section, altering the tube port’s leading surface angle, and introducing new inlet openings, were implemented in five prototypes. After 2D CFD simulations, these prototypes were 3D printed, and experiments were conducted in a wind tunnel across angles from 0° to 55° at three airflow speeds. CFD results indicated increased error with larger inlet diameters and revealed an oscillating error phenomenon for multiple inlet openings. Experimental tests contradicted expected accuracy issues with extended diameters, suggesting superior characteristics at higher angles of attack. An oscillating error of pitot-static tubes with multiple holes was affirmed. The study targeted a pitot-static tube port design with a maximum 5% error in airspeed measurement within attack angles from 0° to 40°, showing promise for vertical takeoff and landing vehicle airspeed measurement during horizontal forward flight.

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Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.

Acknowledgments

The study was performed as part of the project No. SGS23/140/OHK2/2T/16 (Internal grant agency of the Czech Technical University in Prague). The authors would also like to express their gratitude to Pavel Bescec for his valuable consultations in the field of CFD simulations.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 37Issue 4July 2024

History

Received: Nov 15, 2023
Accepted: Feb 12, 2024
Published online: May 13, 2024
Published in print: Jul 1, 2024
Discussion open until: Oct 13, 2024

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Postdoctoral Researcher, Dept. of Air Transport, Czech Technical Univ. in Prague, Horska 2040/3, Prague 128 00, Czech Republic (corresponding author). ORCID: https://orcid.org/0000-0003-1601-9999. Email: [email protected]
Associate Professor, Dept. of Air Transport, Czech Technical Univ. in Prague, Horska 2040/3, Prague 128 00, Czech Republic. ORCID: https://orcid.org/0000-0001-6292-0062. Email: [email protected]
Daniel Urban [email protected]
Ph.D. Candidate, Dept. of Air Transport, Czech Technical Univ. in Prague, Horska 2040/3, Prague 128 00, Czech Republic. Email: [email protected]
Postdoctoral Researcher, Dept. of Air Transport, Czech Technical Univ. in Prague, Horska 2040/3, Prague 128 00, Czech Republic. ORCID: https://orcid.org/0000-0001-8694-4034. Email: [email protected]
Filip Kripsky [email protected]
Postgraduate Student, Dept. of Air Transport, Czech Technical Univ. in Prague, Horska 2040/3, Prague 128 00, Czech Republic. Email: [email protected]
Robert Walton [email protected]
Associate Professor, Dept. of Decision Sciences, College of Business, Embry-Riddle Aeronautical Univ., 1 Aerospace Blvd., Daytona Beach, FL 321 14. Email: [email protected]
Associate Professor, Dept. of Air Transport, Univ. of Zilina, Univerzitna 8215/1, Zilina 010 26, Slovakia. ORCID: https://orcid.org/0000-0002-4726-6987. Email: [email protected]

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