Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels
By: Rolla B. Boughan and George W. Baab
Contributors: Baab, George W.; United States. National Advisory Committee for Aeronautics; Langley Aeronautical Laboratory
Series: Wartime Report / National Advisory Committee for Aeronautics -- no. L204; Wartime Reports (United States. National Advisory Committee for Aeronautics) -- no. L204.
Publisher: National Advisory Committee for Aeronautics
Published: 1944
Place of publication: Washington, D.C
Language: eng
ISBN-13: 9781680156492
Subjects: Aluminum alloys; Plates (Engineering); Strains and stresses; Buckling (Mechanics); Airplanes; Materials; Charts, diagrams; Aluminium; Alliages; Plaques (Ingénierie); Contraintes (Mécanique); Flambage (Résistance des matériaux); Avions; Matériaux; Tableaux, graphiques; Aluminum alloy; Stress; Strain; Buckling; Warping; Diagrams
Other titles: NACA Wartime Reports. Series L.
Description: Charts are presented for the calculation of the critical compressive stress - the stress at which local instability occurs - for idealized web- and T-stiffened panels, and examples of the use of the charts are given.
Notes: NACA Wartime Report L-204.

Originally issued as NACA as Advance Restricted Report L4H29 (August 1944).

Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.

Includes bibliographical references.