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An airfoil flutter model suspension system to accommodate large static transonic airloads [[electronic resource] /] / Wilmer H. Reed, III
| An airfoil flutter model suspension system to accommodate large static transonic airloads [[electronic resource] /] / Wilmer H. Reed, III |
| Autore | Reed Wilmer H |
| Pubbl/distr/stampa | Newport News, VA : , : DEI-Tech, Inc. |
| Descrizione fisica | 1 online resource (36 pages) : illustrations |
| Collana |
NASA contractor report
NASA-CR-177998 |
| Soggetto topico |
Airfoils
Blowdown wind tunnels Flutter analysis Pressure distribution Static pressure Supercritical airfoils Transonic wind tunnels Two dimensional flow |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701788903321 |
Reed Wilmer H
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| Newport News, VA : , : DEI-Tech, Inc. | ||
| 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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Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods / / Gregory P. Herrick
| Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods / / Gregory P. Herrick |
| Autore | Herrick Gregory Paul <1972-> |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2014 |
| Descrizione fisica | 1 online resource (17 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Turbomachinery
Flutter analysis Inlet flow Computational fluid dynamics Aeroelasticity |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703769103321 |
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Herrick Gregory Paul <1972->
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Basis function approximation of transonic aerodynamic influence coefficient matrix [[electronic resource] /] / Wesley W. Li and Chan-gi Pak
| Basis function approximation of transonic aerodynamic influence coefficient matrix [[electronic resource] /] / Wesley W. Li and Chan-gi Pak |
| Autore | Li Wesley W |
| Pubbl/distr/stampa | Edwards, CA : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , [2011] |
| Descrizione fisica | 1 online resource (17 pages) : illustrations |
| Altri autori (Persone) | PakChan-gi <1956-> |
| Collana | NASA/TM |
| Soggetto topico |
Matrices (mathematics)
Transonic flow Aerodynamic coefficients Design optimization Approximation Flutter analysis Influence coefficient Prediction analysis techniques Unsteady aerodynamics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701851203321 |
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Li Wesley W
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| Edwards, CA : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Developing uncertainty models for robust flutter analysis using ground vibration test data / / Starr Potter and Rick Lind
| Developing uncertainty models for robust flutter analysis using ground vibration test data / / Starr Potter and Rick Lind |
| Autore | Potter Starr |
| Pubbl/distr/stampa | Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , April 2001 |
| Descrizione fisica | 1 online resource (16 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Flutter analysis
Ground tests Dynamic structural analysis Dynamic response Mathematical models |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706597803321 |
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Potter Starr
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| Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , April 2001 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Flutter analysis of a transonic fan / / R. Srivastava [and three others]
| Flutter analysis of a transonic fan / / R. Srivastava [and three others] |
| Autore | Srivastava R. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2002 |
| Descrizione fisica | 1 online resource (8 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aeroelasticity
Flutter analysis Transonic flow Turbofans Aerodynamic configurations Scale models |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705667903321 |
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Srivastava R.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Flutter analysis of the Shuttle tile overlay repair concept [[electronic resource] /] / Kim S. Bey ... [and others]
| Flutter analysis of the Shuttle tile overlay repair concept [[electronic resource] /] / Kim S. Bey ... [and others] |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2007] |
| Descrizione fisica | 1 online resource (13 pages) : illustrations |
| Altri autori (Persone) | BeyKim S. <1960-> |
| Collana | NASA/TM |
| Soggetto topico |
Flutter analysis
Turbulent flow Spray characteristics Jet engine fuels Reaction kinetics Hydrocarbons Sulfur dioxides Nitrogen oxides Exhaust emission Fuel injection |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697063303321 |
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2007] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Flutter and forced response analyses of cascades using a two-dimensional linearized Euler solver / / T.S.R. Reddy and R. Srivastava, O. Mehmed
| Flutter and forced response analyses of cascades using a two-dimensional linearized Euler solver / / T.S.R. Reddy and R. Srivastava, O. Mehmed |
| Autore | Reddy T. S. R. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 1999 |
| Descrizione fisica | 1 online resource (25 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Euler equations of motion
Cascade flow Flutter analysis Aeroelasticity Nonlinear equations |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706131103321 |
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Reddy T. S. R.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Harmonic balance computations of fan aeroelastic stability [[electronic resource] /] / Milind A. Bakhle, T.S.R. Reddy ; prepared for the International Forum on Aeroelasticity and Structural Dynamics (IFASD 2009) cosponsored by CEAS and AIAA, Seattle, Washington, June 21-25, 2009
| Harmonic balance computations of fan aeroelastic stability [[electronic resource] /] / Milind A. Bakhle, T.S.R. Reddy ; prepared for the International Forum on Aeroelasticity and Structural Dynamics (IFASD 2009) cosponsored by CEAS and AIAA, Seattle, Washington, June 21-25, 2009 |
| Autore | Bakhle Milind A |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
| Descrizione fisica | 1 online resource (13 pages) : illustrations (color) |
| Altri autori (Persone) | ReddyT. S. R |
| Collana | NASA/TM |
| Soggetto topico |
Reynolds averaging
Flutter analysis Aeroelasticity Flow distribution Three dimensional models Unsteady flow Time domain analysis Three Vibration mode |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910699922903321 |
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Bakhle Milind A
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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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An interactive software for conceptual wing flutter analysis and parametric study / / Vivek Mukhopadhyay
| An interactive software for conceptual wing flutter analysis and parametric study / / Vivek Mukhopadhyay |
| Autore | Mukhopadhyay Vivek |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 1996 |
| Descrizione fisica | 1 online resource (16 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Aerodynamics
Computer programs Flexible wings Flutter analysis Gyration Torsion |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707834303321 |
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Mukhopadhyay Vivek
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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