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Design and implementation of an internal stress wave force balance in a shock tunnel

Robinson, Matthew and Martinez Schramm, Jan and Hannemann, Klaus (2011) Design and implementation of an internal stress wave force balance in a shock tunnel. CEAS Space Journal, Vol. 1 (1-4), pp. 45-57. Springer Verlag Vienna. DOI: 10.1007/s12567-010-0003-5. ISSN 1868-2502.

Full text not available from this repository.

Official URL: http://www.springer.com/astronomy/space+exploration/journal/12567

Abstract

A stress wave internal force balance for the High Enthalpy Shock Tunnel Go¨ttingen (HEG) of the German Aerospace Center (DLR) to measure lift, pitching moment and drag was designed, calibrated and tested. The balance is designed to measure forces in ground based test facilities with test times in the order of milliseconds on models additionally instrumented with surface pressure and wall heat flux gauges from angles of attack of -40 to 20. Experiments in HEG were performed on a 303 mm long, 10 half angle blunt cone at angles of attack from -20 to 0. The tests were conducted utilizing two different operating conditions at total specific enthalpies of 3.0 and 3.5 MJ/kg and dynamic pressures of 30 and 72 kPa. The performance of the balance was assessed by comparing the measured force and moment coefficients with computational fluid dynamics (CFD) predictions.

Document Type:Article
Additional Information:Published online: 10.08.2010, Online ISSN: 1868-2510
Title:Design and implementation of an internal stress wave force balance in a shock tunnel
Authors:
AuthorsInstitution or Email of Authors
Robinson, MatthewUNSPECIFIED
Martinez Schramm, JanJan.Martinez@dlr.de
Hannemann, KlausKlaus.Hannemann@dlr.de
Date:2011
Journal or Publication Title:CEAS Space Journal
Refereed publication:Yes
In Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:Vol. 1
DOI:10.1007/s12567-010-0003-5
Page Range:pp. 45-57
Publisher:Springer Verlag Vienna
ISSN:1868-2502
Status:Published
Keywords:Stress wave force balance Shock tunnel Blunt cone Short duration ground testing
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - Grundlagen Raumtransport - Anlagen und Messtechnik (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Dagmar Brennecke-Hosseinzadeh
Deposited On:08 Oct 2010 09:06
Last Modified:04 Apr 2013 16:23

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