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Application of two linear boundary layer stability codes to flight tests with a natural laminar flow wing glove on a Transport aircraft

Riedel, H. (2017) Application of two linear boundary layer stability codes to flight tests with a natural laminar flow wing glove on a Transport aircraft. Other. DLR-Interner Bericht. DLR-IB-AS-BS-2017-97, 113 S.

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Item URL in elib:https://elib.dlr.de/115891/
Document Type:Monograph (DLR-Interner Bericht, Other)
Title:Application of two linear boundary layer stability codes to flight tests with a natural laminar flow wing glove on a Transport aircraft
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Riedel, H.hansgeorg.riedel (at) dlr.deUNSPECIFIED
Date:2017
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:113
Status:Published
Keywords:Natural laminar flow wing glove, Boundary layer stability Analysis, Tollmien-Schlichting instability, crossflow instability, SALLY code, COSAL code, flight tests, Transport aircraft
Department:AS-TFZ
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Seyfried, Beate
Deposited On:22 Nov 2017 15:22
Last Modified:22 Nov 2017 15:22

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