Validated feasibility study of integrally stiffened metallic fuselage panels for reducing manufacturing costs (NASA CR-)

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Validated feasibility study of integrally stiffened metallic fuselage panels for reducing manufacturing costs (NASA CR-) (ID: B0006RI30G)	Description and Photos \| More ads in Turbo Prop

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Ad Format	Sell
Date of placing	2008-11-28 To expiration: 5 days
Availability	Whole World
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Description and Photos

Validated feasibility study of integrally stiffened metallic fuselage panels for reducing manufacturing costs (NASA CR-)

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