Flow visualization in a chemical laser cavity by pulsed laser holography. Technical report
Technical Report
·
OSTI ID:7185162
This report presents test results of flow visualization in a chemical laser cavity. Holograms were recorded of supersonic flow from a two-dimensional slit nozzle during test runs of HF or DF lasing. Laser cavity pressure was nominally 2 torr. Holographic reconstruction gave schlierens and shadowgraphs which were used to qualitatively define Mach numbers and nozzle exit plane boundary layers.
- Research Organization:
- Army Missile Research Development and Engineering Lab., Redstone Arsenal, Ala. (USA). Propulsion Directorate
- OSTI ID:
- 7185162
- Report Number(s):
- AD-A-015557; RK-75-9
- Country of Publication:
- United States
- Language:
- English
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