@manual{
	titlea = "Prof.",
	vornamea = "Christian",
	namea = "Kähler",
	departmenta = "Fakultät für Luft- und Raumfahrttechnik",
	institutea = "LRT 9 - Institut für Raumfahrttechnik und Weltraumnutzung",
	titleb = "",
	vornameb = "",
	nameb = "",
	departmentb = "",
	instituteb = "",
	titlec = "",
	vornamec = "",
	namec = "",
	departmentc = "",
	institutec = "",
	external-funds = "EU FP7",
	company = "",
	project-title = "Advanced Flow Diagnostics for Aeronautical Research",
	project-abstract = "The objective of AFDAR is to develop, assess and demonstrate new image-based experimental technologies

for the analysis of aerodynamic systems and aerospace propulsion components. The main development

focus is on new three-dimensional methods based on Particle Image Velocimetry (PIV) to measure the flow

field around aircraft components, and on the high-speed version of the planar technique for the analysis in

time-resolved regime of transient/unsteady aerodynamic problems. The progress beyond the state of the art with

respect to current technologies is summarized by three aimed breakthroughs: 1) three-dimensional volumetric

measurements over wings and airfoils;  2) time-resolved measurements and aerodynamic analysis several

orders of magnitude faster than today;  3) turbulence characterization in aerodynamics wind-tunnels at resolution

orders of magnitude higher than today by Long-Range Micro-PIV. The project ultimately aims to support the

design of better aircraft and propulsion systems by enabling the designer to use experimental data during

the development cycle of unprecedented completeness and quality. The work also covers the simultaneous

application of PIV-based techniques and other methods to determine aeroacoustic noise emissions from airframe

and to improve combustion processes to lower NOx, CO2 and soot emissions from engines.",
	proj-beginn = "01.10.2010",
	proj-end = "31.10.2013",
	forschungszentrum = ""
}