Flat sheet metal girder with very thin metal web : Part 3 : Sheet metal girders with spars resistant to bending - the stress in uprights - diagonal tension fields

This report continues the work presented in NACA-TM 605 and expands the scope to include the change in specific number of wrinkles from direction x to z, so that b and f become variable in direction z. Moreover, it seems likely that b and f increase from the edge toward the center if the sheet is in...

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Bibliographic Details
Main Author: Wagner, Herbert, 1900-1982.
Corporate Author: United States. National Advisory Committee for Aeronautics.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1931]
Series: Technical memorandums (United States. National Committee for Aeronautics) ; no. 606.
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ISBN: 9781680156584
1680156586
Physical Description: 1 online resource (39, [8] pages) : illustrations

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Summary: This report continues the work presented in NACA-TM 605 and expands the scope to include the change in specific number of wrinkles from direction x to z, so that b and f become variable in direction z. Moreover, it seems likely that b and f increase from the edge toward the center if the sheet is infinitely thin.
Item Description: "February, 1931."
NACA TM No. 606.
Translated from Zeitschrift fur Flugtechnik und Motorluftschiffahrt. Vol. 20, No. 11, pp. 281-284, June 14, and No. 12, pp. 306-314, June 28, 1929, by the National Advisory Committee for Aeronautics.
Bibliography: Includes bibliographical references.
ISBN: 9781680156584
1680156586
Access: Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty