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Advanced turboprop vibratory characteristics [[electronic resource] ] : final report / / A. V. Srinivasan, G. B. Fulton
| Advanced turboprop vibratory characteristics [[electronic resource] ] : final report / / A. V. Srinivasan, G. B. Fulton |
| Autore | Srinivasan A. V (Amruthur V.) |
| Pubbl/distr/stampa | East Hartford, CT : , : United Technologies Research Center |
| Descrizione fisica | 1 online resource (1 volumes (various pagings)) : digital, PDF file |
| Altri autori (Persone) | FultonG. B |
| Collana | NASA contractor report |
| Soggetto topico |
Data bases
Dynamic structural analysis Prop-fan technology Propeller fans Vibrational stress |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Advanced turboprop vibratory characteristics |
| Record Nr. | UNINA-9910699748503321 |
Srinivasan A. V (Amruthur V.)
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| East Hartford, CT : , : United Technologies Research Center | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model / / Aparajit J. Mahajan [and three others]
| Aeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model / / Aparajit J. Mahajan [and three others] |
| Autore | Mahajan Aparajit J (Aparajit Jagannath) |
| Pubbl/distr/stampa | Washington, D.C. : , : NASA, , April 1992 |
| Descrizione fisica | 1 online resource (approximately 14 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Prop-fan technology
Flutter Cruise missiles |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717012003321 |
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Mahajan Aparajit J (Aparajit Jagannath)
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| Washington, D.C. : , : NASA, , April 1992 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Analysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed [[electronic resource] /] / by Arthur F. Smith
| Analysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed [[electronic resource] /] / by Arthur F. Smith |
| Autore | Smith Arthur F |
| Pubbl/distr/stampa | Windsor Locks, Conn. : , : Hamilton Standard Division, United Technologies Corporation |
| Descrizione fisica | 1 online resource (x, 101/102 pages) : illustrations |
| Collana | NASA CR |
| Soggetto topico |
Aerodynamic stability
Dynamic response Dynamic structural analysis Evaluation Prop-fan technology Turboprop engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701902203321 |
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Smith Arthur F
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| Windsor Locks, Conn. : , : Hamilton Standard Division, United Technologies Corporation | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Analysis and test evaluation of the dynamic stability of three advanced turboprop models at zero forward speed [[electronic resource] /] / by Arthur F. Smith
| Analysis and test evaluation of the dynamic stability of three advanced turboprop models at zero forward speed [[electronic resource] /] / by Arthur F. Smith |
| Autore | Smith Arthur F |
| Pubbl/distr/stampa | Windsor Locks, Conn. : , : Hamilton Standard Division, United Technologies Corporation |
| Descrizione fisica | 1 online resource (ix/x, 114 pages) : illustrations |
| Collana | NASA CR |
| Soggetto topico |
Dynamic stability
Evaluation Prop-fan technology Turboprop engines Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701902003321 |
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Smith Arthur F
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| Windsor Locks, Conn. : , : Hamilton Standard Division, United Technologies Corporation | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Dynamic open-rotor composite shield impact test report / / Silvia Seng [and six others]
| Dynamic open-rotor composite shield impact test report / / Silvia Seng [and six others] |
| Autore | Seng Silvia |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 2015 |
| Descrizione fisica | 1 online resource (62 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Commercial aircraft
Prop-fan technology Impact tests Failure analysis Photogrammetry |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704276203321 |
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Seng Silvia
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Evaluation of MARC for the analysis of rotating composite blades / / Karen F. Bartos and Michael A. Ernst
| Evaluation of MARC for the analysis of rotating composite blades / / Karen F. Bartos and Michael A. Ernst |
| Autore | Bartos Karen F. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , March 1993 |
| Descrizione fisica | 1 online resource (24 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Blades
Composite materials Centrifugal force Eigenvalues Finite element method Nonlinearity Prop-fan technology |
| Soggetto genere / forma | Online resources. |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707954403321 |
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Bartos Karen F.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , March 1993 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Evaluation of propfan propulsion applied to general aviation [[electronic resource] /] / by R.W. Awker
| Evaluation of propfan propulsion applied to general aviation [[electronic resource] /] / by R.W. Awker |
| Autore | Awker R. W |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , [1985] |
| Descrizione fisica | 1 online resource (ix, 138 pages) : illustrations |
| Collana | NASA-CR |
| Soggetto topico |
Aerodynamic characteristics
Aircraft construction materials Aircraft design Aircraft safety Civil aviation Cost effectiveness Fuel consumption Performance tests Prop-fan technology Propeller efficiency Propulsion system performance Structural design criteria |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910700871803321 |
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Awker R. W
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , [1985] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Large-scale advanced prop-fan (LAP) ptich change actuator and control design report [[electronic resource] /] / by Robert A. Schwartz, Paul Carvalho, Mark J. Cutler
| Large-scale advanced prop-fan (LAP) ptich change actuator and control design report [[electronic resource] /] / by Robert A. Schwartz, Paul Carvalho, Mark J. Cutler |
| Autore | Schwartz Robert A |
| Pubbl/distr/stampa | [Cleveland, Ohio] : , : National Aeronautics and Space Administration, Lewis Research Center, , [1986] |
| Descrizione fisica | 1 online resource (1 volumes (various pagings)) : digital, PDF file |
| Altri autori (Persone) |
CarvalhoPaul
CutlerMark J |
| Collana | NASA CR |
| Soggetto topico |
Design analysis
Hydraulic control Prop-fan technology Structural design Variable pitch propellers |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Large-scale advanced prop-fan |
| Record Nr. | UNINA-9910700188403321 |
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Schwartz Robert A
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| [Cleveland, Ohio] : , : National Aeronautics and Space Administration, Lewis Research Center, , [1986] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984 [[electronic resource] /] / D. Parzych, [S. Cohen, A. Shenkman]
| Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984 [[electronic resource] /] / D. Parzych, [S. Cohen, A. Shenkman] |
| Autore | Parzych David J |
| Pubbl/distr/stampa | [Washington, DC] : , : [National Aeronautics and Space Administration] |
| Descrizione fisica | iv, 56 pages : illustrations |
| Altri autori (Persone) |
CohenS
ShenkmanArieh L |
| Collana | NASA contractor report |
| Soggetto topico |
Aerodynamic characteristics
Aerodynamic noise Acoustic properties Blade tips High speed Mach number Prop-fan technology Propeller fans Power efficiency Weight (mass) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Large-scale Advanced Propfan |
| Record Nr. | UNINA-9910700283803321 |
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Parzych David J
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| [Washington, DC] : , : [National Aeronautics and Space Administration] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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NPSS multidisciplinary integration and analysis [[electronic resource] /] / Edward J. Hall ... [and others]
| NPSS multidisciplinary integration and analysis [[electronic resource] /] / Edward J. Hall ... [and others] |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2006] |
| Descrizione fisica | 1 online resource (x, 172 pages) : illustrations |
| Altri autori (Persone) | HallEdward J |
| Collana | NASA/CR- |
| Soggetto topico |
Turbomachinery
Computational fluid dynamics Structural analysis Prop-fan technology Compressor blades Guide vanes Iteration |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697084903321 |
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2006] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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