1. Laser propagation through an absorbing transonic flow
- Author
-
David C. Smith and Robert T. Brown
- Subjects
Physics ,Shock wave ,Supersonic wind tunnel ,Physics and Astronomy (miscellaneous) ,Shock (fluid dynamics) ,business.industry ,Mechanics ,symbols.namesake ,Optics ,Mach number ,Schlieren ,symbols ,business ,Transonic ,Physics::Atmospheric and Oceanic Physics ,Beam (structure) ,Schlieren photography - Abstract
Experiments were carried out to investigate the propagation of a cw CO2 laser beam through an absorbing slightly supersonic flow. A 500‐W CO2 beam was propagated through a small blow‐down wind tunnel operating with an air/SF6 mixture in order to simulate a high‐power beam propagating through the atmosphere. A collinear schlieren system was used to observe the density gradients caused by the absorbed power. Large density gradients were observed at a Mach number of 1.17; however, they were not shock initiated and their magnitude was not inconsistent with a heat‐balance analysis. Under the conditions of the experiment no shock waves were observed, even though their occurrence was predicted by a simple one‐dimensional analysis. From this study it is concluded that shock waves will not occur under most conditions encountered by high‐power cw CO2 laser radiation in the atmosphere. The presence of subshock density gradients and their effect on the propagating beam require further study.
- Published
- 1974