Computational Design and Analysis of a Transonic Natural Laminar Flow Wing for a Wind Tunnel Model

A natural laminar flow (NLF) wind tunnel model has been designed and analyzed for a wind tunnel test in the National Transonic Facility (NTF) at the NASA Langley Research Center. The NLF design method is built into the CDISC design module and uses a Navier-Stokes flow solver, a boundary layer profil...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Lynde, Michelle N., Campbell, Richard L.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Aerodynamics
Online-Zugang:	Volltext bestellen
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