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Influence of a Microramp Array on a Hypersonic Shock-Wave/Turbulent Boundary-Layer Interaction

; ; ;

In
AIAA journal 59(6), Seiten/Artikel-Nr.:1924-1939

ImpressumReston, Va. [u.a.] : American Institute of Aeronautics and Astronautics

ISSN1533-385X

Online
DOI: 10.2514/1.J059925


Einrichtungen

  1. Lehrstuhl für Strömungslehre und Aerodynamisches Institut (415110)


Thematische Einordnung (Klassifikation)
DDC: 380


Dokumenttyp
Journal Article

Format
online

Sprache
English

Anmerkung
Peer reviewed article

Externe Identnummern
WOS Core Collection: WOS:000658581200003

Interne Identnummern
RWTH-2021-05835
Datensatz-ID: 820803

Beteiligte Länder
Germany, USA

Lizenzstatus der Zeitschrift

 GO

Medline ; Clarivate Analytics Master Journal List ; Current Contents - Engineering, Computing and Technology ; Ebsco Academic Search ; Essential Science Indicators ; IF < 5 ; JCR ; NationallizenzNationallizenz ; SCOPUS ; Science Citation Index Expanded ; Web of Science Core Collection
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The record appears in these collections:
Document types > Articles > Journal Articles
Faculty of Mechanical Engineering (Fac.4)
Public records
Publications database
415110
 Record created 2021-06-21, last modified 2024-03-07
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