Accurate time-resolved static pressure measurements are key to characterizing the freestream thermodynamic state in hypervelocity reflected shock tunnels. A series of three static pressure probes were built for use in the T5 Free-Piston Shock Tunnel at the California Institute of Technology based on the design of Behrens. Simultaneously, Tunable Diode Laser Absorption Spectroscopy (TDLAS) was used to infer static pressure from the pressure broadening of absorption features in nitric oxide rovibrational spectroscopic transitions from the mid-infrared fundamental band. Test conditions covered stagnation enthalpies from 8 to 16 MJ/kg and freestream pressures from 7 to 27 kPa. The pressure measurements from the first two static probe generations agreed in magnitude with the TDLAS pressure within error, but showed very different temporal responses due to the slower time responses of the two probes. Subsequently, a quicker time response static probe was designed and deployed in T5 in the 8 MJ/kg and 16 MJ/kg conditions. The pressure traces from the new probe agreed well in both magnitude and temporal response with the TDLAS-inferred pressure in both conditions. In addition, the new probe was able to resolve subtle temporal differences between differently tailored versions of the same condition. The updated static probe design allows for simultaneous high-frequency pressure measurement with test models and increases confidence in pressure broadening TDLAS measurements in high-enthalpy ground test facilities.
Published January 2024
| Published
Conference Paper
High-Frequency Static Pressure Measurements in the T5 Reflected Shock Tunnel
Abstract
Copyright and License
© 2024 by the American Institute of Aeronautics and Astronautics, Inc.
Acknowledgement
This work was supported in part by AFOSR FA9550-21-1-0080 with Drs. Ivett Leyva and Sarah Popkin as programofficers, and FA9550-23-1-0446 with Dr. Michael Berman as program officer. The authors would like to thank Ali Kiani,Brandon Nilles, Bahram Valiferdowsi, and Noel Esparza-Duran for assistance in fabricating parts for the experimentalsetup. Additionally, the authors thank Alex Acosta, Michael Stramenga, and Jorge Rodriguez Gutierrez for helping withsetup, alignment, and facility turnaround for these experiments. The authors also thank Dr. Julian Girard for his manycontributions to the TDLAS sensor design.
Additional details
- United States Air Force Office of Scientific Research
- FA9550-21-1-0080
- United States Air Force Office of Scientific Research
- FA9550-23-1-0446
- Caltech groups
- GALCIT
- Other Numbering System Name
- AIAA Paper
- Other Numbering System Identifier
- 2024-2884