Integral airframe structures (IAS)
Subtitle: validated feasibility study of integrally stiffened metallic fuselage panels for reducing manufacturing costs
By: J. Munroe, K. Wilkins and M. Gruber.
Contributors: Gruber, M. L.; Wilkins, K. E.; Boeing Company. Commercial Airplane Group.; Langley Research Center.
Series: NASA/CR : -- 2000-209337; NASA contractor report -- NASA CR-2000-209337.
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
Subjects: Airframes -- Materials -- Fatigue.; Airplanes -- Fuselage -- Design and construction.; Costs, Industrial.
Other titles: Validated feasibility study of integrally stiffened metallic fuselage panels for reducing manufacturing costs
Notes: "May 2000."

Includes bibliographical references.

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