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Document type:
Konferenzbeitrag
Contribution type:
Textbeitrag / Aufsatz
Author(s):
Pfnür, S.; Breitsamter, C.
Title:
Outboard Split Flap Aerodynamics of a Flying Wing Configuration
Abstract:
The yaw-control device of a low-aspect-ratio flying-wing configuration is investigated. The novel layout of the so-called outboard split flap with its hinge-line along the swept leading edge is designed to achieve beneficial yaw-control characteristics. Force and moment measurements as well as stereo particle image velocimetry measurements allow for the analysis of the aerodynamics of the control device. Additionally, Unsteady Reynolds-Averaged Navier-Stokes simulations are performed a...     »
Keywords:
Aerodynamics, Directional Controllability; Flying Wing; Wind Tunnel; CFD
Dewey Decimal Classification:
620 Ingenieurwissenschaften
Book / Congress title:
Congress of the International Council of the Aeronautical Sciences [31´st, Belo Horizonte, 2018]
Volume:
ICAS 2018_0069, Code 143115
Date of congress:
9.-14.9.
Year:
2018
Print-ISBN:
978-393218288-4
Reviewed:
ja
Language:
en
WWW:
https://www.icas.org/ICAS_ARCHIVE/ICAS2018/data/preview/ICAS2018_0069.htm
TUM Institution:
Lehrstuhl für Aerodynamik
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