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Analysis and sizing for transient thermal heating of insulated aerospace vehicle structures / / Max L. Blosser
| Analysis and sizing for transient thermal heating of insulated aerospace vehicle structures / / Max L. Blosser |
| Autore | Blosser Max L |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , 2012 |
| Descrizione fisica | 1 online resource (50 pages) : color illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Aerospace vehicles
Insulation Transient heating Aircraft structures Transient response Mathematical models Hypersonic vehicles Size (dimensions) |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702342603321 |
Blosser Max L
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , 2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Design and verification guidelines for vibroacoustic and transient environments [[electronic resource]]
| Design and verification guidelines for vibroacoustic and transient environments [[electronic resource]] |
| Pubbl/distr/stampa | [Marshall Space Flight Center, Ala.] : , : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, Component Analysis Branch, Systems Dynamics Laboratory, , [1986] |
| Descrizione fisica | iv, 23 pages : digital, PDF file |
| Collana | NASA technical memorandum |
| Soggetto topico |
Acoustic measurement
Design analysis Proving Random vibration Shock spectra Structural vibration Transient response Vibration tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697712003321 |
| [Marshall Space Flight Center, Ala.] : , : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, Component Analysis Branch, Systems Dynamics Laboratory, , [1986] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Development of higher-order modal methods for transient thermal and structural analysis [[electronic resource] /] / Charles J. Camarda and Raphael T. Haftka
| Development of higher-order modal methods for transient thermal and structural analysis [[electronic resource] /] / Charles J. Camarda and Raphael T. Haftka |
| Autore | Camarda Charles J |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1989] |
| Descrizione fisica | 37 pages : digital, PDF file |
| Altri autori (Persone) | HaftkaRaphael T |
| Collana | NASA technical memorandum |
| Soggetto topico |
Damping
Modal response Problem solving Stiffness matrix Structural analysis Thermal analysis Transient response |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697919903321 |
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Camarda Charles J
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1989] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Dynamic simulation of a wave rotor topped turboshaft engine / / R.B. Greendyke, D.E. Paxson, M.T. Schobeiri
| Dynamic simulation of a wave rotor topped turboshaft engine / / R.B. Greendyke, D.E. Paxson, M.T. Schobeiri |
| Autore | Greendyke Robert B. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1997 |
| Descrizione fisica | 1 online resource (9 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Turboshafts
Inlet pressure Dynamic characteristics Flow velocity Fuel flow Transient response Computerized simulation |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707633903321 |
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Greendyke Robert B.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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An introduction to transient engine applications using the numerical propulsion system simulation (NPSS) and MATLAB® / / Jeffrey C. Chin [and three others]
| An introduction to transient engine applications using the numerical propulsion system simulation (NPSS) and MATLAB® / / Jeffrey C. Chin [and three others] |
| Autore | Chin Jeffrey C (Jeffrey Chuan-che) |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , January 2016 |
| Descrizione fisica | 1 online resource (19 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Transient response
Engine design Numerical analysis Computerized simulation Mathematical models |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Introduction to transient engine applications using the numerical propulsion system simulation |
| Record Nr. | UNINA-9910704381303321 |
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Chin Jeffrey C (Jeffrey Chuan-che)
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , January 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Reducing conservatism in aircraft engine response using conditionally active min-max limit regulators / / Ryan D. May, Sanjay Garg
| Reducing conservatism in aircraft engine response using conditionally active min-max limit regulators / / Ryan D. May, Sanjay Garg |
| Autore | May Ryan D. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (10 pages) : illustrations |
| Collana | NASA/TM 2012-217814 |
| Soggetto topico |
Commercial aircraft
Aircraft control Control systems design Engine control Sequential control Transient response |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704624303321 |
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May Ryan D.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A transient response method for linear coupled substructures / / J.R. Admire and J.A. Brunty
| A transient response method for linear coupled substructures / / J.R. Admire and J.A. Brunty |
| Autore | Admire J. R. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, , December 1989 |
| Descrizione fisica | 1 online resource (v, 20 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Discrete functions
Linear systems Loads (forces) Mathematical models Numerical integration Transient response |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705755203321 |
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Admire J. R.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, , December 1989 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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