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The Potential of Ultrasonically Absorptive TPS Materials for Hypersonic Vehicles

Wagner, Alexander and Wartemann, Viola and Hannemann, Klaus and Kuhn, Markus and Dittert, Christian (2015) The Potential of Ultrasonically Absorptive TPS Materials for Hypersonic Vehicles. American Institute of Aeronautics and Astronautics. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015-07-06 - 2015-07-09, Glasgow, Scotland. doi: 10.2514/6.2015-3576.

Full text not available from this repository.

Official URL: http://arc.aiaa.org/doi/10.2514/6.2015-3576

Abstract

The potential of ultrasonically absorptive carbon fiber reinforced carbon (C/C) based materials for passive boundary layer transition control on hypersonic flight vehicles is investigated. Based on previous studies on C/C, optimized C/C based materials are developed and studied with respect to their temperature stability and ultrasonic absorption properties at hypersonic flight regimes of interest. Generic vehicle shapes providing an essentially two dimensional flow field allowing the second mode instability to be the dominant boundary layer instability are studied using an engineering approach. Furthermore, the study provides an overview on the test procedures established in DLR to assess the ultrasonic absorption properties of porous materials and to experimentally investigate the impact of potential candidates on the boundary layer transition process.

Item URL in elib:https://elib.dlr.de/97486/
Document Type:Conference or Workshop Item (Speech)
Additional Information:AIAA-2015-3576
Title:The Potential of Ultrasonically Absorptive TPS Materials for Hypersonic Vehicles
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Wagner, AlexanderUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Wartemann, ViolaUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Hannemann, KlausUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Kuhn, MarkusUNSPECIFIEDhttps://orcid.org/0000-0002-0633-2327UNSPECIFIED
Dittert, ChristianBT-RSIUNSPECIFIEDUNSPECIFIED
Date:2015
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI:10.2514/6.2015-3576
Page Range:pp. 1-11
Publisher:American Institute of Aeronautics and Astronautics
Series Name:Conference Proceedings online
Status:Published
Keywords:hypersonic boundary layer transition, carbon-carbon, passive transition control, UAC, ultrasonically absorptive coating, second mode damping
Event Title:20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Event Location:Glasgow, Scotland
Event Type:international Conference
Event Start Date:6 July 2015
Event End Date:9 July 2015
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Anlagen u. Messtechnik (old)
Location: Braunschweig , Göttingen , Stuttgart
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Institute of Structures and Design > Space System Integration
Deposited By: Micknaus, Ilka
Deposited On:30 Sep 2015 10:27
Last Modified:24 Apr 2024 20:03

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