DocumentCode
2903041
Title
Nonintrusive measurements in fluid dynamic flows from Mach 0.0005 to 14
Author
Seibert, G.L.
Author_Institution
WL/FIMN, Wright Patterson AFB, OH, USA
fYear
1991
fDate
27-31 Oct 1991
Firstpage
74
Lastpage
81
Abstract
A concentrated effort was begun to introduce nonintrusive diagnostics systems into the test facilities wherever possible. The author describes the efforts made, the results obtained, and the plans underway to achieve the goal of providing state-of-the-art diagnostics instrumentation in all the operating facilities. A survey of the work that has been accomplished and the ongoing development is reviewed, including a low-speed large water tunnel and some development concepts being studied
Keywords
aerospace test facilities; flow measurement; fluid dynamics; aerospace testing; fluid dynamic flows; nonintrusive diagnostics; test facilities; water tunnel; Aerodynamics; Fluid dynamics; Foot; Glass; Holography; Optical design; Optical interferometry; Pulse measurements; Test facilities; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation in Aerospace Simulation Facilities, 1991. ICIASF '91 Record., International Congress on
Conference_Location
Rockville, MD
Type
conf
DOI
10.1109/ICIASF.1991.186227
Filename
186227
Link To Document