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Aeroelastic deformation [[electronic resource]] : adaptation of wind tunnel measurement concepts to full-scale vehicle flight testing / / Alpheus W. Burner, William A. Lokos, Danny A. Barrows
| Aeroelastic deformation [[electronic resource]] : adaptation of wind tunnel measurement concepts to full-scale vehicle flight testing / / Alpheus W. Burner, William A. Lokos, Danny A. Barrows |
| Autore | Burner Alpheus W |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2005] |
| Descrizione fisica | 1 online resource (19 pages) : illustrations |
| Altri autori (Persone) |
LokosWilliam A
BarrowsDanny A |
| Collana | NASA TM- |
| Soggetto topico |
Aeroelasticity
Deflection Wings Flight tests |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aeroelastic deformation |
| Record Nr. | UNINA-9910697197003321 |
Burner Alpheus W
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2005] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aileron and Kruger nose flaps effectiveness measured on an oblique wing / / Edward J. Hopkins and George H. Lovette
| Aileron and Kruger nose flaps effectiveness measured on an oblique wing / / Edward J. Hopkins and George H. Lovette |
| Autore | Hopkins Edward J. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , March 1977 |
| Descrizione fisica | 1 online resource (iv, 272 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Ailerons
Wings Airplanes - Wings |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716975003321 |
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Hopkins Edward J.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , March 1977 | ||
| 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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Computational icing risk analysis of the D8 "Double Bubble" aircraft / / Christopher E. Porter and Mark G. Potapczuk
| Computational icing risk analysis of the D8 "Double Bubble" aircraft / / Christopher E. Porter and Mark G. Potapczuk |
| Autore | Porter Christopher E. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2018 |
| Descrizione fisica | 1 online resource (30 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Aircraft icing Contours Ice prevention Wings |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910711870203321 |
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Porter Christopher E.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2018 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Correlation of structural analysis and test results for the McDonnell Douglas stitched/RFI all-composite wing stub box / / John T. Wang [and three others]
| Correlation of structural analysis and test results for the McDonnell Douglas stitched/RFI all-composite wing stub box / / John T. Wang [and three others] |
| Autore | Wang John T. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 1996 |
| Descrizione fisica | 1 online resource (33 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Composite structures
Finite element method Graphite-epoxy composites Wings Strain distribution Bending Commercial aircraft Aircraft structures |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Correlation of structural analysis and test results for the McDonnell Douglas stitched resin film infusion all-composite wing stub box |
| Record Nr. | UNINA-9910707862103321 |
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Wang John T.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Deformed shape calculation of a full-scale wing using fiber optic strain data from a ground loads test / / Christine V. Jutte [and five others]
| Deformed shape calculation of a full-scale wing using fiber optic strain data from a ground loads test / / Christine V. Jutte [and five others] |
| Autore | Jutte Christine V. |
| Pubbl/distr/stampa | Edwards, CA : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , [2011] |
| Descrizione fisica | 1 online resource (vi, 50 pages) : color illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Deformation
Ground tests Shapes Wings Fiber optics Strain distribution Full scale tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701909803321 |
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Jutte Christine V.
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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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Design verification and fabrication of active control systems for the DAST ARW-2 high aspect ratio wing / / C.R. McGehee
| Design verification and fabrication of active control systems for the DAST ARW-2 high aspect ratio wing / / C.R. McGehee |
| Autore | McGehee C. R. |
| Pubbl/distr/stampa | Wichita, KS : , : The Boeign Co. |
| Descrizione fisica | 1 online resource (2 volumes) : illustrations |
| Collana | NASA contractor report |
| Soggetto topico |
Active control
Aerodynamic configurations Automatic flight control Design analysis Fabrication High aspect ratio Proving Structural analysis Wings |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | pt. 1 [Without special title] -- pt. 2. Appendices. |
| Record Nr. | UNINA-9910704917903321 |
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McGehee C. R.
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| Wichita, KS : , : The Boeign Co. | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Effect of Kruger nose flaps on the experimental force and moment characteristics of an oblique wing / / Edward J. Hopkins and George H. Lovette
| Effect of Kruger nose flaps on the experimental force and moment characteristics of an oblique wing / / Edward J. Hopkins and George H. Lovette |
| Autore | Hopkins Edward J. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , July 1976 |
| Descrizione fisica | 1 online resource (iv, 204 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Wings
Oblique wings Airplanes - Wings, Swept-back Flaps (Airplanes) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716975203321 |
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Hopkins Edward J.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , July 1976 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet / / Michael Papadakis [and six others]
| Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet / / Michael Papadakis [and six others] |
| Autore | Papadakis Michael |
| Pubbl/distr/stampa | Cleveland Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2002 |
| Descrizione fisica | 1 online resource (430 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Water
Drops (liquids) Impingement Airfoils Wings Engine inlets |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705699503321 |
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Papadakis Michael
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| Cleveland Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Finite element analysis and test results comparison for the hybrid wing body center section test article / / Adam Przekop [and three others]
| Finite element analysis and test results comparison for the hybrid wing body center section test article / / Adam Przekop [and three others] |
| Autore | Przekop Adam |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2016 |
| Descrizione fisica | 1 online resource (viii, 106 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Critical loading
Finite element method Strain measurement Structural stability Wings |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706249303321 |
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Przekop Adam
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
-
Wings
(30)
- Aerodynamics (6)
- Design analysis (5)
- Aerodynamic configurations (4)
- Finite element method (4)