Validated feasibility study of integrally stiffened metallic fuselage panels for reducing manufacturing costs
Subtitle: cost assessment of manufacturing/design concepts
By: S. Metschan.
Contributors: Boeing Company. Commercial Airplane Group.; Langley Research Center.
Series: NASA CR : -- 2000-209343; NASA contractor report -- NASA CR-2000-209343.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from NASA Center for AeroSpace Information
Published: 2000
Place of publication: Hampton, Va; Hanover, MD
Language: eng
Number of pages: 19
Subjects: Airframes -- Materials -- Fatigue.; Airplanes -- Fuselage -- Design and construction.; Costs, Industrial.
Notes: "February 2000."

Includes bibliographical references.

Prepared by Boeing Commercial Airplane Group for Langley Research Center NAS1-20014 and NAS1-20267 522-12-51-01