A shielded fine-wire probe for rapid measurement of total temperature in high-speed flows
- 1 April 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (4), 425-428
- https://doi.org/10.2514/3.30297
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Influence of measured freestream disturbances on hypersonic boundary-layer transitionAIAA Journal, 1970
- Use of a pulse heated fine wire probe for the measurement of total temperature in shock driven facilitiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Design and Calibration of Stagnation Temperature Probes for Use at High Supersonic Speeds and Elevated TemperaturesJournal of Applied Physics, 1954