High-Speed Photoinstrumentation for a Hypersonic Wind Tunnel
The application of high-speed cameras and short-duration light sources to measure pressures, forces and flow patterns in a high-velocity (up to Mach 25) short-duration (less than 15 msec) wind tunnel are described. Details of the measuring techniques are given, including the optical systems, lighting, data reduction procedures, measurement accuracies and synchronization methods.
- Print ISSN
- 0361-4573
- Published
- 1964-08
- Content type
- Original Research
- DOI
- 10.5594/J07201
Download the PDF
or become a SMPTE member today to access the
article.
Become a SMPTE
member today to access the article.