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Analysis of apex seal friction power loss in rotary engines [[electronic resource] /] / Robert F. Handschuh, A. Karl Owen
| Analysis of apex seal friction power loss in rotary engines [[electronic resource] /] / Robert F. Handschuh, A. Karl Owen |
| Autore | Handschuh Robert F |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
| Descrizione fisica | 1 online resource (15 pages) : illustrations (color) |
| Altri autori (Persone) | OwenA. Karl |
| Collana | NASA/TM |
| Soggetto topico |
Internal combustion engines
Rotary engines Internal pressure Friction factor Seals (stoppers) Kinematics |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910699921603321 |
Handschuh Robert F
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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PRSEUS pressure cube test data and response / / Andrew E. Lovejoy
| PRSEUS pressure cube test data and response / / Andrew E. Lovejoy |
| Autore | Lovejoy Andrew E. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2013 |
| Descrizione fisica | 1 online resource (236 unnumbered pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Blended-wing-body configurations
Composite materials Commercial aircraft Panels Rods Loads (forces) Internal pressure Structural weight Weight reduction |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Pultruded Rod Stitched Efficient Unitized Structure pressure cube test data and response |
| Record Nr. | UNINA-9910704630103321 |
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Lovejoy Andrew E.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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