Fabrication and evaluation of superplastically formed/weld-brazed corrugated compression panels with beaded webs / / Dick M. Royster [and four others]
| Fabrication and evaluation of superplastically formed/weld-brazed corrugated compression panels with beaded webs / / Dick M. Royster [and four others] |
| Autore | Royster Dick M. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , November 1985 |
| Descrizione fisica | 1 online resource (28 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Fabrication
Brazing Beads Titanium alloys Superplasticity Airplanes - Fuselage - Design and construction Sheet-metal, Corrugated - Testing |
| Soggetto genere / forma | Online resources. |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709734103321 |
Royster Dick M.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , November 1985 | ||
| Lo trovi qui: Univ. Federico II | ||
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Shear lag in corrugated sheets used for the chord member of a box beam / / by Joseph S. Newell and Eric Reissner
| Shear lag in corrugated sheets used for the chord member of a box beam / / by Joseph S. Newell and Eric Reissner |
| Autore | Newell Joseph Shipley <1897-> |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1941 |
| Descrizione fisica | 1 online resource (51 pages, 20 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Sheet-metal, Corrugated - Testing
Strains and stresses Aerofoils |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717300903321 |
Newell Joseph Shipley <1897->
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1941 | ||
| Lo trovi qui: Univ. Federico II | ||
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