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Visualization of a hypersonic boundary layer on a transition cone

Laurence, Stuart and Wagner, Alexander and Ozawa, Hiroshi and Hannemann, Klaus (2014) Visualization of a hypersonic boundary layer on a transition cone. American Institute of Aeronautics and Astronautics. AIAA Aviation Technology, Integration, and Operations Conference, 16. – 20. June 2014, Atlanta, GA, USA.

Full text not available from this repository.

Official URL: http://arc.aiaa.org | DOI: 10.2514/6.2014-3110

Abstract

A series of experiments is performed in the High Enthalpy shock tunnel Göttingen (HEG) to investigate instability development and transition in the hypersonic boundary layer of a slender, zero-incidence cone. Two schlieren-based-techniques - pulsed-laser schlieren and schlieren deflectometry - are employed over a range of conditions, both lowand high-enthalpy. Pulsed-laser schlieren, a development of an earlier technique, provides a detailed picture of instability growth and breakdown, both in an average sense and for individual wave packets. Measurements on a smooth cone surface and a naturally porous, ceramic surface are compared. The deflectometry technique allows approximate amplification rates to be determined. Finally, fast-response temperature sensitive paint measurements are performed to obtain quantitative heat-transfer information on the unsteady transitional region of the cone.

Item URL in elib:https://elib.dlr.de/88674/
Document Type:Conference or Workshop Item (Speech)
Additional Information:AIAA-2014-3110, 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, DOI: 10.2514/6.2014-3110
Title:Visualization of a hypersonic boundary layer on a transition cone
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Laurence, Stuartstuartl (at) umd.eduUNSPECIFIED
Wagner, Alexanderalexander.wagner (at) dlr.deUNSPECIFIED
Ozawa, Hiroshihiroshi.ozawa (at) dlr.deUNSPECIFIED
Hannemann, Klausklaus.hannemann (at) dlr.deUNSPECIFIED
Date:2014
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-22
Publisher:American Institute of Aeronautics and Astronautics
Series Name:Conference Proceedings online
Status:Published
Keywords:HEG, Transition, Cone, Schlieren, boundary-layer
Event Title:AIAA Aviation Technology, Integration, and Operations Conference
Event Location:Atlanta, GA, USA
Event Type:international Conference
Event Dates:16. – 20. June 2014
Organizer:AIAA
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: Micknaus, Ilka
Deposited On:18 Jul 2014 10:24
Last Modified:20 Oct 2014 16:56

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