K.S.G. Krishnan, O. Bertram

The objective of this paper is to analyze the system aspects for installation of an active hybrid laminar flow control system with a chamberless suction nose on the leading edge of the vertical tail plane of a mid-range transport aircraft. The inputs from various disciplines which are important from systems perspective are extracted, and the interfaces between various disciplines are drawn. A study is conducted to assess the proposed systems architectures, and a trade-off analysis is subsequently performed.

Deutscher Luft- und Raumfahrtkongress 2017, München

Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2017

Conference Paper

englisch

21,0 x 29,7 cm, 7 Seiten

urn:nbn:de:101:1-201712088141

Hybrid-Laminar Flow Control, TuLAM

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08.12.2017