| Description |
1 online resource (39, [8] pages) : illustrations |
| Series |
Technical memorandums / National Advisory Committee for Aeronautics ; 606 |
|
Technical memorandums (United States. National Committee for Aeronautics) ; no. 606
|
| 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 |
| Notes |
"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 |
| Notes |
Master and use copy. Digital master created according to Technical Guidelines for Digitizing Archival Materials for Electronic Access. U.S. National Archives and Records Administration, 2004. http://www.archives.gov/preservation/technical/guidelines.html TxDN |
|
Print version record |
|
digitized 2011 University of North Texas committed to preserve pda TXdn |
| Subject |
Sheet-metal.
|
|
Girders.
|
|
Mathematics.
|
|
Struts (Engineering)
|
|
Strains and stresses.
|
|
Bending.
|
|
sheet metal.
|
|
mathematics.
|
|
applied mathematics.
|
|
strain.
|
|
stress.
|
|
Bending
|
|
Girders
|
|
Mathematics
|
|
Sheet-metal
|
|
Strains and stresses
|
|
Struts (Engineering)
|
| Form |
Electronic book
|
| Author |
United States. National Advisory Committee for Aeronautics.
|
| ISBN |
9781680156584 |
|
1680156586 |
|
