A Method of calculating the compressive strength of Z-stiffened panels that develop local instability

• Main Author: Gallaher, George L. (Author)
• Corporate Author: United States. National Advisory Committee for Aeronautics
• Other Authors: Boughan, Rolla B.
• Format: Electronic eBook
• Language: English
• Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
• Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1482.
• Subjects: Plates (Engineering); Strains and stresses.; Buckling (Mechanics); Mathematical analysis.; elektronické knihy; electronic books
• ISBN: 9781680156102; 1680156101
• Physical Description: 1 online resource (15 pages) : illustrations, tables
• Abstract: A method, based on the elastic theory for plate buckling and test results for 24S-T aluminum-alloy Z-stiffened panels, is shown for calculating the compressive strength of Z-stiffened panels that develop local instability. This method can be used to calculate the critical compressive stress above, as well as within, the elastic range. For stresses above three-fourths the compressive yield stress the method can be used for the approximate determination of the average compressive stress at maximum load.
• Item Description: "November 1947."; NACA TN No. 1482.
• Access: Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty