Temperature- and Pressure-Sensitive Paint Measurements in Short-Duration Hypersonic Flow
- 1 April 2001
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 39 (4) , 654-659
- https://doi.org/10.2514/2.1358
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Pressure-sensitive paint measurements in a shock tubeExperiments in Fluids, 2000
- Temperature- and pressure-sensitive paint measurements in short-duration hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- Treating temperature-sensitivity effects of pressure-sensitive paint measurementsExperiments in Fluids, 1998
- Temperature- and Pressure-Sensitive Luminescent Paints in AerodynamicsApplied Mechanics Reviews, 1997
- Step response of pressure-sensitive paintsAIAA Journal, 1996
- Heat transfer measurement on a waverider at Mach 10 using fluorescent paintJournal of Thermophysics and Heat Transfer, 1995
- Pressure-sensitive paint in aerodynamic testingExperimental Thermal and Fluid Science, 1995
- Submillisecond response times of oxygen-quenched luminescent coatingsReview of Scientific Instruments, 1993
- Aerodynamic applications of pressure sensitive paintAIAA Journal, 1993