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Aeroelastic tailoring via tow steered composites / / Bret K. Stanford, Christine V. Jutte
Aeroelastic tailoring via tow steered composites / / Bret K. Stanford, Christine V. Jutte
Autore Stanford Bret K.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2014
Descrizione fisica 1 online resource (25 pages) : color illustrations
Collana NASA/TM
Soggetto topico Aeroelasticity
Laminates
Stiffness matrix
Transverse loads
High aspect ratio
Aerodynamic loads
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702734303321
Stanford Bret K.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Cause and cure: deterioration in accuracy of CFD simulations with use of high-aspect-ratio triangular/tetrahedral grids / / Sin-Chung Chang, Chau-Lyan Chang, Balaji Shankar Venkatachari
Cause and cure: deterioration in accuracy of CFD simulations with use of high-aspect-ratio triangular/tetrahedral grids / / Sin-Chung Chang, Chau-Lyan Chang, Balaji Shankar Venkatachari
Autore Chang Sin-Chung
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2017
Descrizione fisica 1 online resource (39 pages) : illustrations
Collana NASA/TM
Soggetto topico Computational fluid dynamics
High aspect ratio
High Reynolds number
Navier-Stokes equation
Space-time CE/SE method
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Cause and cure
Record Nr. UNINA-9910706177203321
Chang Sin-Chung  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2017
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber / / Mary F. Wadel
Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber / / Mary F. Wadel
Autore Wadel Mary F.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , June 1997
Descrizione fisica 1 online resource (11 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Combustion chambers
High aspect ratio
Cooling
Channels
Computer programs
Design
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910708661203321
Wadel Mary F.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , June 1997
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Comparison of Theodorsen's unsteady aerodynamic forces with double lattice generalized aerodynamic forces / / Boyd Perry, III
Comparison of Theodorsen's unsteady aerodynamic forces with double lattice generalized aerodynamic forces / / Boyd Perry, III
Autore Perry Boyd
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2017
Descrizione fisica 1 online resource (30 pages) : illustrations
Collana NASA/TM
Soggetto topico Unsteady aerodynamics
Slender wings
Aerodynamic forces
High aspect ratio
Mach number
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706501803321
Perry Boyd  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2017
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
McGehee C. R.  
Wichita, KS : , : The Boeign Co.
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Jet surface interaction noise in a high aspect ratio rectangular exhaust / / Abbas Khavaran
Jet surface interaction noise in a high aspect ratio rectangular exhaust / / Abbas Khavaran
Autore Khavaran Abbas <1953->
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2017
Descrizione fisica 1 online resource (iii, 29 pages) : color illustrations
Collana NASA contractor report
Soggetto topico Aeroacoustics
Aerodynamic noise
High aspect ratio
Jet aircraft noise
Jet exhaust
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705810603321
Khavaran Abbas <1953->  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2017
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Numerical solution of three-dimensional unsteady transonic flow over wings including viscid/viscous interactions / / D. P. Rizzetta and C. J. Borland
Numerical solution of three-dimensional unsteady transonic flow over wings including viscid/viscous interactions / / D. P. Rizzetta and C. J. Borland
Autore Rizzetta Donald Pasquale <1944->
Pubbl/distr/stampa Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , February 1984
Descrizione fisica 1 online resource (77 pages) : illustrations
Collana NASA/CR
Soggetto topico Potential flow
Flow distribution
High aspect ratio
Swept wings
Shear layers
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Numerical solution of three-dimensional unsteady transonic flow over wings including inviscid/viscous interactions
Record Nr. UNINA-9910709665403321
Rizzetta Donald Pasquale <1944->  
Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , February 1984
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Passive aeroelastic tailoring : final report / / Benjamin Smith [and six others]
Passive aeroelastic tailoring : final report / / Benjamin Smith [and six others]
Autore Smith Benjamin
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , February 2020
Descrizione fisica 1 online resource (various pagings) : color illustrations
Collana NASA/CR
Soggetto topico High aspect ratio
Additive manufacturing
Aircraft design
Slender wings
Steering
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Passive aeroelastic tailoring
Record Nr. UNINA-9910712964503321
Smith Benjamin  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , February 2020
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Recent development in the CESE method for the solution of the Navier-Stokes Equations using unstructured triangular or tetrahedral meshes with high aspect ratio / / Sin-Chung Chang, Chau-Lyan Chang, Joseph C. Yen
Recent development in the CESE method for the solution of the Navier-Stokes Equations using unstructured triangular or tetrahedral meshes with high aspect ratio / / Sin-Chung Chang, Chau-Lyan Chang, Joseph C. Yen
Autore Chang Sin-Chung
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2013
Descrizione fisica 1 online resource (40 pages) : illustrations
Collana NASA/TM
Soggetto topico Space-time CE/SE method
Computational aeroacoustics
Computational fluid dynamics
High aspect ratio
Navier-Stokes equation
Viscous flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Recent development in the Conservation Element and Solution Element method for the solution of the Navier-Stokes equations using unstructured triangular or tetrahedral meshes with high aspect ratio
Record Nr. UNINA-9910702431203321
Chang Sin-Chung  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Slot nozzle effects for reduced sonic boom on a generic supersonic wing section [[electronic resource] /] / Raymond S. Castner ; prepared for the 48th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics Orlando, Florida, January 4-7, 2010
Slot nozzle effects for reduced sonic boom on a generic supersonic wing section [[electronic resource] /] / Raymond S. Castner ; prepared for the 48th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics Orlando, Florida, January 4-7, 2010
Autore Castner Raymond S
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Descrizione fisica 1 online resource (10 pages) : illustrations
Collana NASA TM-
Soggetto topico Exhaust nozzles
Sonic booms
Wing slots
Aircraft control
Computational fluid dynamics
Exhaust gases
Supersonic speed
Mach number
High aspect ratio
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910699548503321
Castner Raymond S  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

Data di pubblicazione