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CFD Analysis of radiative heat loading on hypervelocity re-entry vehicles

Karl, Sebastian and Potter, Daniel and Lambert, Markus and Hannemann, Klaus (2015) CFD Analysis of radiative heat loading on hypervelocity re-entry vehicles. Journal of Spacecraft and Rockets, 52 (1), pp. 63-74. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.A32791 ISSN 0022-4650

Full text not available from this repository.

Official URL: http://arc.aiaa.org/doi/pdf/10.2514/1.A32791

Abstract

Space exploration missions may include atmospheric entries at very high velocities (e.g. sample-return, entries from hyperbolic orbits) or into an atmosphere with highly radiative constituents (e.g. Mars, Titan). The effects of gas radiation in the shock layer and wake flows may become significant at such flight conditions. Hence, accurate CFD analysis of these flows requires adequate modeling of the local absorption and emission properties and the energy transport by radiation. This paper presents a brief overview of numerical techniques for the integration of radiation effects in atmospheric entry vehicle simulations, and the subsequent prediction of radiative heat loading. Brief reviews are given of the available models for excited state populations spectral properties and radiative energy transport. Particular emphasis is given to the Monte Carlo transport models which enable accurate solutions on complex grid topologies in a computationally efficient manner.

Item URL in elib:https://elib.dlr.de/93277/
Document Type:Article
Additional Information:Published online: 23 April 2014, January - February 2015
Title:CFD Analysis of radiative heat loading on hypervelocity re-entry vehicles
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Karl, Sebastiansebastian.karl (at) dlr.deUNSPECIFIED
Potter, Danieldaniel.potter (at) dlr.deUNSPECIFIED
Lambert, Markusmarkus.lambert (at) dlr.deUNSPECIFIED
Hannemann, Klausklaus.hannemann (at) dlr.deUNSPECIFIED
Date:2015
Journal or Publication Title:Journal of Spacecraft and Rockets
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:52
DOI :10.2514/1.A32791
Page Range:pp. 63-74
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0022-4650
Status:Published
Keywords:CFD, Radiation, Hypersonics, Re-entry
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 - Numerische Verfahren und Simulation
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Micknaus, Ilka
Deposited On:08 Dec 2014 12:41
Last Modified:08 Mar 2018 18:45

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