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PROBES IN TRANSONIC FLOW

Kost, Friedrich (2008) PROBES IN TRANSONIC FLOW. XIX Biannual Symposium on Measuring Techniques in Turbomachinery, April 2008, Brussels, Belgium.

Full text not available from this repository.

Abstract

A constraint exists for intrusive probes in transonic flow which leads to a complete insensitivity to static pressure at Mach number Ma=1. Nearby Mach number unity different types of probes are affected more or less by the reduced sensitivity to static pressure or Mach number. In this paper three types of probes are compared and it is shown that the reduced sensitivity near Ma=1 causes large errors when the flow Mach number is determined by a conventional probe. A closer look onto the pressure distribution of a blunt body reveals that only the front part of a probe is subject to the constraint while base pressure is not affected. Therefore a base pressure tapping was added to a conventional Cobra type probe. The new probe was calibrated in the Probe Calibration Facility of DLR Göttingen at a wide range of Mach numbers and at two Reynolds numbers.

Item URL in elib:https://elib.dlr.de/83090/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:PROBES IN TRANSONIC FLOW
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Kost, FriedrichAT-TUUNSPECIFIED
Date:2008
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:pneumatic probes, transonic flow, calibration, base pressure
Event Title:XIX Biannual Symposium on Measuring Techniques in Turbomachinery
Event Location:Brussels, Belgium
Event Type:international Conference
Event Dates:April 2008
HGF - Research field:Energy
HGF - Program:Efficient Energy Conversion and Use (old)
HGF - Program Themes:Power Plants (old)
DLR - Research area:Energy
DLR - Program:E VG - Combustion and Gas Turbine Technologies
DLR - Research theme (Project):E - Gasturbine (old)
Location: Göttingen
Institutes and Institutions:Institute of Propulsion Technology > Turbine
Deposited By: Giess, Dr.-Ing. Peter-Anton
Deposited On:25 Jun 2013 14:58
Last Modified:25 Jun 2013 14:58

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