Header menu link for other important links
X
Reduction of Induced Drag in Con guration Flight using Wing Twist at Post-Stall Angles of Attack
Gunasekaran M,
Published in American Institute of Aeronautics and Astronautics
2016
Abstract

Abstract is unavailable for this paper.

About the journal
JournalData powered by Typeset54th AIAA Aerospace Sciences Meeting
PublisherData powered by TypesetAmerican Institute of Aeronautics and Astronautics
ISSN0001-1452
Impact Factor1.868
Open AccessNo
Citation Styleunsrt
Sherpa RoMEO Archiving PolicyGreen