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| Experimental Aircraft Flutter Stability Analysis for the Hyper-X Hypersonic Vehicle Case Study Overview
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Document Date: 2014-07-02 20:42:31

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File Size: 177,69 KB

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City

Diego / /

Company

Orbital Sciences Corp / ATA Engineering Inc. / /

IndustryTerm

space travel / /

Organization

National Aeronautics and Space Administration / /

Person

Virginia Ph / /

/

Position

Panel model for flutter analysis / /

ProvinceOrState

California / /

URL

www.ata-e.com / /

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