L-infinity-Optimal Feed-forward Gust Load Alleviatkion Design for a large Blended Wing Body Airliner

Title:: L-infinity-Optimal Feed-forward Gust Load Alleviatkion Design for a large Blended Wing Body Airliner
Document type:: Konferenzbeitrag
Author(s):: Wildschek, A.; Hanis, T.; Stroscher, F.
Keywords:: Gust Load Alleviation Design; Blended Wing Body Airliner
Dewey Decimal Classification:: 620 Ingenieurwissenschaften
Book / Congress title:: EUCASS
Year:: 2011
Language:: en
TUM Institution:: Lehrstuhl für Leichtbau
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