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Hypersonic Shock Wave Boundary Layer Interaction Studies on a Flat Plate at Elevated Surface Temperature

Wagner, Alexander and Schramm, M. and Hickey, Jean Pierre and Hannemann, Klaus (2016) Hypersonic Shock Wave Boundary Layer Interaction Studies on a Flat Plate at Elevated Surface Temperature. 22nd International Shock Interaction Symposium, 04.-08. Juli 2016, Glasgow, England.

Full text not available from this repository.

Official URL: http://www.gla.ac.uk/conferences/shockinteractionsymposium/

Abstract

Experimental shock wave boundary layer interactions (SWBLI) on a flat plate model with deflectable flap and variable surface temperature were studied in the DLR High Enthalpy Shock Tunnel Göttingen (HEG) at Mach 7.4 and 6.65x106 m−1 unit Reynolds number. The wind tunnel model used in the scope of the study was equipped with an internal heating element allowing for variable surface temperatures up to 800 K. The model consists of an unheated flap which can be deflected in the range of 0◦, 15◦ and 30◦, a heatable flat plate and an exchangeable leading edge. The latter is passively heated through the contact to the heated model section. At the hinge line a gap of 0.2 mm was realized between the flap and flat plate. In the scope of the study the effects caused by leading edge bluntness, flap deflection angel, gap opening and surface temperature on the shock wave boundary layer interaction were investigated. Additional attention was paid to the laminar turbulent boundary layer transition process.

Item URL in elib:https://elib.dlr.de/105618/
Document Type:Conference or Workshop Item (Speech)
Title:Hypersonic Shock Wave Boundary Layer Interaction Studies on a Flat Plate at Elevated Surface Temperature
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Wagner, AlexanderAlexander.Wagner (at) dlr.deUNSPECIFIED
Schramm, M.Martinez.Schramm (at) dlr.deUNSPECIFIED
Hickey, Jean PierreMechanical and Mechatronics Engineering, University of Waterloo, CanadaUNSPECIFIED
Hannemann, Klausklaus.hannemann (at) dlr.deUNSPECIFIED
Date:2016
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Hypersonic Boundary-Layer Transition, HEG, SWBLI, heated wind tunnel model
Event Title:22nd International Shock Interaction Symposium
Event Location:Glasgow, England
Event Type:international Conference
Event Dates:04.-08. Juli 2016
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Anlagen u. Messtechnik
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Bachmann, Barbara
Deposited On:02 Dec 2016 13:14
Last Modified:12 Jan 2017 12:01

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