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A back face strain compliance expression for the compact tension specimen / / William T. Riddell and Robert S. Piascik
| A back face strain compliance expression for the compact tension specimen / / William T. Riddell and Robert S. Piascik |
| Autore | Riddell William T. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 1998 |
| Descrizione fisica | 1 online resource (8 pages) : illustrations |
| Collana | NASA TM |
| Soggetto topico |
Stress intensity factors
Crack propagation Tensile stress Stress distribution Fracture mechanics Cracking (fracturing) |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705850503321 |
Riddell William T.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 1998 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Balancing dynamic strength of spur gears operated at extended center distance / / Hsiang Hsi Lin [and three others]
| Balancing dynamic strength of spur gears operated at extended center distance / / Hsiang Hsi Lin [and three others] |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center |
| Descrizione fisica | 1 online resource (6 pages) : illustrations |
| Collana |
NASA technical memorandum
Army Research Laboratory technical report |
| Soggetto topico |
Gears
Gear teeth Dynamic models Stress distribution |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706516803321 |
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A clamped rectangular plate containing a crack [[electronic resource] /] / Renji Tang and F. Erdogan
| A clamped rectangular plate containing a crack [[electronic resource] /] / Renji Tang and F. Erdogan |
| Autore | Tang Renji |
| Pubbl/distr/stampa | Bethlehem, Pa. : , : Lehigh University, Department of Mechanical Engineering and Mechanics |
| Descrizione fisica | 1 online resource (21 pages, 5 unnumbered pages) : illustrations |
| Altri autori (Persone) | ErdoganF (Fazil) |
| Collana | NASA contractor report |
| Soggetto topico |
Crack geometry
Crack propagation Metal plates Stress distribution |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702002203321 |
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Tang Renji
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| Bethlehem, Pa. : , : Lehigh University, Department of Mechanical Engineering and Mechanics | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The effect of interface roughness and oxide film thickness on the inelastic response of thermal barrier coatings to thermal cycling / / Marek-Jerzy Pindera, Jacob Aboudi, Steven M. Arnold
| The effect of interface roughness and oxide film thickness on the inelastic response of thermal barrier coatings to thermal cycling / / Marek-Jerzy Pindera, Jacob Aboudi, Steven M. Arnold |
| Autore | Pindera M.-J (Marek-Jerzy), <1951-> |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 1999 |
| Descrizione fisica | 1 online resource (16 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Interfaces
Oxide films Thickness Surface roughness Temperature effects Stress distribution Film thickness |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706280303321 |
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Pindera M.-J (Marek-Jerzy), <1951->
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Free-edge delamination : laminate width and loading conditions effects / / P.L.N. Murthy and C.C. Chamis
| Free-edge delamination : laminate width and loading conditions effects / / P.L.N. Murthy and C.C. Chamis |
| Autore | Murthy P. L. N. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1987 |
| Descrizione fisica | 1 online resource (26 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Axial stress
Delaminating Fiber composites Finite element method Interlayers Stress distribution |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Free-edge delamination |
| Record Nr. | UNINA-9910705703503321 |
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Murthy P. L. N.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1987 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Impact and penetration of thin aluminum 2024 flat panels at oblique angles of incidence / / Charles R. Ruggeri [and four others]
| Impact and penetration of thin aluminum 2024 flat panels at oblique angles of incidence / / Charles R. Ruggeri [and four others] |
| Autore | Ruggeri Charles R. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2015 |
| Descrizione fisica | 1 online resource (99 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aluminum
Finite element method Computational mechanics Stress distribution Impact tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704381703321 |
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Ruggeri Charles R.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Local strain redistribution corrections for a simplified inelastic analysis procedure based on an elastic finite-element analysis / / Albert Kaufman and Shoi Y. Hwang
| Local strain redistribution corrections for a simplified inelastic analysis procedure based on an elastic finite-element analysis / / Albert Kaufman and Shoi Y. Hwang |
| Autore | Kaufman Albert <1928-> |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , March 1985 |
| Descrizione fisica | 1 online resource (11 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Aircraft gas-turbines - Materials
Elastic analysis (Engineering) Finite element method Strains and stresses Cyclic loads Inelastic stress Nonlinear equations Stress distribution Stress-strain relationships |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709797103321 |
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Kaufman Albert <1928->
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , March 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A new look at numerical analyses of free-edge stresses in composite laminates / / I.S. Raju, J.D. Whitcomb, J.G. Goree
| A new look at numerical analyses of free-edge stresses in composite laminates / / I.S. Raju, J.D. Whitcomb, J.G. Goree |
| Autore | Raju I. S. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 |
| Descrizione fisica | 1 online resource (34 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Continuum mechanics
Elastic properties Graphite-epoxy composites Laminates Stress distribution |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707467203321 |
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Raju I. S.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Non-classical stress concentration behavior in a radially stretched hyperelastic sheet containing a circular hole / / William L. Ko, Shun-Fat Lung
| Non-classical stress concentration behavior in a radially stretched hyperelastic sheet containing a circular hole / / William L. Ko, Shun-Fat Lung |
| Autore | Ko William L. |
| Pubbl/distr/stampa | Edwards, CA : , : National Aeronautics and Space Administration, Armstrong Flight Research Center, , August 2017 |
| Descrizione fisica | 1 online resource (vi, 27 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Axial stress
Elastic sheets Hole geometry (mechanics) Stress concentration Stress distribution |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706125203321 |
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Ko William L.
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| Edwards, CA : , : National Aeronautics and Space Administration, Armstrong Flight Research Center, , August 2017 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Progressive fracture of fiber composite build-up structures / / Pascal K. Gotsis and C.C. Chamis, Levon Minnetyan
| Progressive fracture of fiber composite build-up structures / / Pascal K. Gotsis and C.C. Chamis, Levon Minnetyan |
| Autore | Gotsis Pascal K. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , September 1996 |
| Descrizione fisica | 1 online resource (14 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Fiber composites
Composite structures Fracturing Bending Graphite-epoxy composites Finite element method Stress distribution |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705786203321 |
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Gotsis Pascal K.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , September 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
-
Stress distribution
(14)
- Finite element method (4)
- Axial stress (2)
- Crack propagation (2)
- Fiber composites (2)