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Flutter of Winged Reentry Space Vehicles Affected by an Elastic Attachment in Launching Configuration

Transactions of the Japan Society for Aeronautical and Space Sciences- Japan

doi 10.2322/tjsass.46.262

Full Text

Abstract

Available in

Categories

SpacePlanetary ScienceAerospace Engineering

Date

January 1, 2004

Authors

Atsushi KandaTetsuhiko Ueda

Publisher

Japan Society for Aeronautical and Space Sciences


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