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Engineering Transition Prediction of a Hypersonic Axisymmetric Boundary Layer

Stilla, J. (1994) Engineering Transition Prediction of a Hypersonic Axisymmetric Boundary Layer. Journal of Aircraft, pp. 1358-1364.

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for the design of future hypersonic aerospace planes the estimation of maximum heat loads plays an important role. It especially depends on boundary-layer transition for which engineering tools are required at the present time an estimation of transition location in hyper-sonic flow still has to rely on either empirical correlations based on mean-flow properties, or on local, linear stability analysis in conjunction with the e**N method. In any case,a laminar, steady meanflow has to be computed. Each modification of the design requires repeated transition pre- diction and, therefore, repeated computation of laminar, steady mean flows. Because solutions of the full Navier-Stokes equations are verytime consuming, and therefore expensive, one has to choose an approp-riate approximation of these equations. Two common approximations are the parabolized Navier-Stokes equations (PNS) and the thin-layer Navier-Stokes equations (TLNS).

Item URL in elib:https://elib.dlr.de/36295/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=1994,
Title:Engineering Transition Prediction of a Hypersonic Axisymmetric Boundary Layer
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Journal or Publication Title:Journal of Aircraft
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:Yes
Page Range:pp. 1358-1364
Series Name:Vol. 31 No.6
Keywords:hypersonic boundarz layers, blunt core, second-order boundarylayer theory, linear local stability analysis, entropy layer
HGF - Research field:UNSPECIFIED
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:UNSPECIFIED
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - Grundlagen Raumtransport - Anlagen und Messtechnik (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: DLR-Beauftragter, elib
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:05

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