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