DocumentCode
2902894
Title
Investigation on optimizing the design process of multi-hole pressure probes for transonic flow with panel methods
Author
Depolt, Th ; Koschel, W.
Author_Institution
Inst. for Jet Propulsion & Turbomachinery, Tech. Univ. of Aachen, Germany
fYear
1991
fDate
27-31 Oct 1991
Firstpage
1
Lastpage
9
Abstract
Developments made at the Institute of Jet Propulsion and Turbomachinery of the Technical University of Aachen on the topic of miniaturized multihole pressure probes to be utilized in transonic turbine flows are presented. The main emphasis is on the numerical description of the flow around the probe head. A very efficient tool, the panel method, was used to calculate the pressure distribution on the surface. By the aid of this method the design process of a pneumatic multihole pressure probe can be supported. The influence of some geometry variations on the flow around the probe head is investigated, and the probe coefficients are presented and discussed
Keywords
flow measurement; flowmeters; pressure transducers; probes; design optimisation; flow interference; miniaturised probe; multi-hole pressure probes; numerical modelling; pneumatic probe; probe head; transonic flow; turbine flows; turbomachinery; Design optimization; Fluid flow measurement; Interference; Probes; Process design; Propulsion; Shafts; Testing; Turbines; Turbomachinery;
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.1991.186218
Filename
186218
Link To Document