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Aerodynamic Performance Analysis of a Hypersonic Inlet Isolator Using Computation and Experiment

Reinartz, B. and Herrmann, C. and Ballmann, J. and Koschel, W. (2003) Aerodynamic Performance Analysis of a Hypersonic Inlet Isolator Using Computation and Experiment. Journal of Propulsion and Power, 19 (5), pp. 868-875.

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Item URL in elib:https://elib.dlr.de/1667/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=2003,
Title:Aerodynamic Performance Analysis of a Hypersonic Inlet Isolator Using Computation and Experiment
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Reinartz, B.RWTH AachenUNSPECIFIED
Herrmann, C.RWTH AachenUNSPECIFIED
Ballmann, J.RWTH AachenUNSPECIFIED
Koschel, W.UNSPECIFIEDUNSPECIFIED
Date:2003
Journal or Publication Title:Journal of Propulsion and Power
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Volume:19
Page Range:pp. 868-875
Status:Published
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):E - no assignment
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: Lohmiller, Monika
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 14:06

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