Supersonic and transonic Mach probe for calibration control in the Trisonic Wind Tunnel
A supersonic and high speed transonic Pitot Prandtl is described as it can be implemented in the Trisonic Wind Tunnel for calibration and verification of Mach number precision. A new calculation method for arbitrary precision Mach numbers is proposed and explained. The probe is specially designed fo...
| Main Author: | |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2017-12-01
|
| Series: | INCAS Bulletin |
| Subjects: | |
| Online Access: | http://bulletin.incas.ro/files/panait_m__vol_9_iss_4__mod__final.pdf |