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Aeroelastic analyses of the SemiSpan Supersonic Transport (S⁴T) wind tunnel model at Mach 0.95 / / Jiyoung Hur
| Aeroelastic analyses of the SemiSpan Supersonic Transport (S⁴T) wind tunnel model at Mach 0.95 / / Jiyoung Hur |
| Autore | Hur Jiyoung |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 2014 |
| Descrizione fisica | 1 online resource (64 pages) : color illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Aeroelasticity
Dynamic pressure Flutter Transonic flow Structured grids (mathematics) Dynamic structural analysis |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aeroelastic analyses of the SemiSpan Supersonic Transport |
| Record Nr. | UNINA-9910702780703321 |
Hur Jiyoung
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 2014 | ||
| 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 of an unswept propfan blade with a semiempirical dynamic stall model / / T.S.R. Reddy, K.R.V. Kaza
| Analysis of an unswept propfan blade with a semiempirical dynamic stall model / / T.S.R. Reddy, K.R.V. Kaza |
| Autore | Reddy T. S. R. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , January 1989 |
| Descrizione fisica | 1 online resource (approiximately 22 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Stalling
Flutter Aerodynamic stalling Propellers, Aerial - Testing Flutter (Aerodynamics) Stalling (Aerodynamics) - Simulation methods |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717043203321 |
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Reddy T. S. R.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , January 1989 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Application of approximate unsteady aerodynamics for flutter analysis [[electronic resource] /] / Chan-gi Pak and Wesley W. Li
| Application of approximate unsteady aerodynamics for flutter analysis [[electronic resource] /] / Chan-gi Pak and Wesley W. Li |
| Autore | Pak Chan-gi |
| Pubbl/distr/stampa | Edwards, Calif. : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , [2010] |
| Descrizione fisica | 1 online resource (20 pages) : illustrations |
| Altri autori (Persone) | LiWesley W |
| Collana | NASA/TM |
| Soggetto topico |
Aerodynamic coefficients
Aerodynamics Approximation Flutter Flutter analysis Prediction analysis techniques Unsteady aerodynamics Wings |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910699916603321 |
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Pak Chan-gi
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| Edwards, Calif. : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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ASTROP2 users manual : a program for aeroelastic stability analysis of propfans / / T.S.R. Reddy and John M. Lucero
| ASTROP2 users manual : a program for aeroelastic stability analysis of propfans / / T.S.R. Reddy and John M. Lucero |
| Autore | Reddy T. S. R. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , March 1996 |
| Descrizione fisica | 1 online resource (ii, 41 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Aeroelasticity
Aerodynamic forces Finite element method Flutter User manuals (computer programs) Unsteady aerodynamics Contrarotating propellers Computer programs |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | ASTROP2 users manual |
| Record Nr. | UNINA-9910707003103321 |
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Reddy T. S. R.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , March 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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MAVRIC flutter model transonic limit cycle oscillation test / / John W. Edwards [and four others]
| MAVRIC flutter model transonic limit cycle oscillation test / / John W. Edwards [and four others] |
| Autore | Edwards John W. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2001 |
| Descrizione fisica | 1 online resource (15 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Transonic flow
Flutter Wind tunnel models Wing tips Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Models for aeroelastic validation research involving computation flutter model transonic limit cycle oscillation test |
| Record Nr. | UNINA-9910691728603321 |
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Edwards John W.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2001 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Model verification and validation concepts for a probabilistic fracture assessment model to predict cracking of knife edge seals in the space shuttle main engine high pressure oxidizer / / Shantaram S. Pai, David S. Riha
| Model verification and validation concepts for a probabilistic fracture assessment model to predict cracking of knife edge seals in the space shuttle main engine high pressure oxidizer / / Shantaram S. Pai, David S. Riha |
| Autore | Pai Shantaram S. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2013] |
| Descrizione fisica | 1 online resource (9 pages) : illustrations |
| Collana | NASA/TM 2013-217849 |
| Soggetto topico |
Flutter
Cracking (fracturing) Prediction analysis techniques Fracture mechanics Probability theory Proving Fatigue life Fatigue (materials) Mathematical models |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704876303321 |
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Pai Shantaram S.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2013] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Nonlinear aeroelastic analysis of the HIAD TPS coupon in the NASA 8' high temperature tunnel : theory and experiment / / Benjamin D. Goldman, Robert C. Scott, Earl H. Dowell
| Nonlinear aeroelastic analysis of the HIAD TPS coupon in the NASA 8' high temperature tunnel : theory and experiment / / Benjamin D. Goldman, Robert C. Scott, Earl H. Dowell |
| Autore | Goldman Benjamin D. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2014 |
| Descrizione fisica | 1 online resource (44 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Thermal protection
Aerodynamic brakes Aeroelasticity Heat shielding Inflatable structures High temperature tests Flutter |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Nonlinear aeroelastic analysis of the HIAD TPS coupon in the NASA 8' high temperature tunnel |
| Record Nr. | UNINA-9910702659303321 |
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Goldman Benjamin D.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Overview of recent flight flutter testing research at NASA Dryden / / Martin J. Brenner, Richard C. Lind, and David F. Voracek
| Overview of recent flight flutter testing research at NASA Dryden / / Martin J. Brenner, Richard C. Lind, and David F. Voracek |
| Autore | Brenner Martin J. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , April 1997 |
| Descrizione fisica | 1 online resource (27 pages) : illustrations |
| Collana | NASA Technical Memorandum |
| Soggetto topico |
Aeroservoelasticity
Flutter System identification Vibration effects Wavelet analysis |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707009803321 |
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Brenner Martin J.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , April 1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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