An evaluation of the pressure proof test concept for thin sheet 2024-T3 /

An evaluation of the pressure proof test concept for thin sheet 2024-T3 /

Bibliographic Details
Corporate Author: Langley Research Center
Other Authors: Dawicke, D. S.
Format: Government Document Book
Language:English
Published: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
Series:NASA technical memorandum ; 101675.
Subjects:
Airplanes > Fuselage > Testing.
Crack propagation.
Cracks.
Fatigue life.
Fracture mechanics.
Fuselages.
Structural failure.
Transport aircraft.
Description
Item Description:Cover title.
Shipping list no.: 90-0857-M.
"April 1990."
Physical Description:30 pages : illustrations
Also available via Internet from the NASA Technical Report Server web site. Address as of 3/1/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900012108%5F1990012108.pdf; current access available via PURL.
Bibliography:Includes bibliographical references (pages 14-15).