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Computational investigation of novel tip leakage mitigation methods for high pressure turbine blades / / Mounir Ibrahim and Abhinav Gupta, Vikram Shyam
Computational investigation of novel tip leakage mitigation methods for high pressure turbine blades / / Mounir Ibrahim and Abhinav Gupta, Vikram Shyam
Autore Ibrahim Mounir B.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 2014
Descrizione fisica 1 online resource (19 pages) : color illustrations
Collana NASA/TM
Soggetto topico Computational fluid dynamics
Turbine blades
Rotor blades (turbomachinery)
Hole distribution (mechanics)
Hole geometry (mechanics)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910703786003321
Ibrahim Mounir B.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Design evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application / / Ali Abdul-Aziz, George Y. Baaklini, Ramakrishna T. Bhatt
Design evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application / / Ali Abdul-Aziz, George Y. Baaklini, Ramakrishna T. Bhatt
Autore Abdul-Aziz Ali
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2001
Descrizione fisica 1 online resource (15 pages) : color illustrations
Collana NASA/TM
Soggetto topico Silicon nitrides
Finite element method
Thermal stresses
Thermal environments
Hole geometry (mechanics)
Air cooling
Thermodynamic efficiency
Ceramics
Temperature distribution
Stress analysis
Ceramic coatings
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706550203321
Abdul-Aziz Ali  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2001
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Long hole film cooling dataset for CFD development . Part 1 Infrared thermography and thermocouple surveys / / Vikram Shyam [and five others]
Long hole film cooling dataset for CFD development . Part 1 Infrared thermography and thermocouple surveys / / Vikram Shyam [and five others]
Autore Shyam Vikram
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013
Descrizione fisica 1 online resource (40 pages) : color illustrations
Collana NASA/TM
Soggetto topico Reynolds number
Hole geometry (mechanics)
Thermal mapping
Thermography
Infrared imagery
Computational fluid dynamics
Hot-wire anemometers
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702430803321
Shyam Vikram  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Non-classical stress concentration behavior in a radially stretched hyperelastic sheet containing a circular hole / / William L. Ko, Shun-Fat Lung
Non-classical stress concentration behavior in a radially stretched hyperelastic sheet containing a circular hole / / William L. Ko, Shun-Fat Lung
Autore Ko William L.
Pubbl/distr/stampa Edwards, CA : , : National Aeronautics and Space Administration, Armstrong Flight Research Center, , August 2017
Descrizione fisica 1 online resource (vi, 27 pages) : illustrations
Collana NASA/TM
Soggetto topico Axial stress
Elastic sheets
Hole geometry (mechanics)
Stress concentration
Stress distribution
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706125203321
Ko William L.  
Edwards, CA : , : National Aeronautics and Space Administration, Armstrong Flight Research Center, , August 2017
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Spreadsheet calculations for jets in crossflow [[electronic resource]] : opposed rows of inline and staggered holes and single and opposed rows with alternating hole sizes / / James D. Holdeman, James R. Clisset, Jeffrey P. Moder
Spreadsheet calculations for jets in crossflow [[electronic resource]] : opposed rows of inline and staggered holes and single and opposed rows with alternating hole sizes / / James D. Holdeman, James R. Clisset, Jeffrey P. Moder
Autore Holdeman J. D
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Descrizione fisica 1 online resource (33 pages) : illustrations
Altri autori (Persone) ClissetJames R
ModerJeffrey P
Collana NASA/TM-
Soggetto topico Cross flow
Hole geometry (mechanics)
Gas turbine engines
Combustion chambers
Mathematical models
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Spreadsheet calculations for jets in crossflow
Record Nr. UNINA-9910699793503321
Holdeman J. D  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control / / Scott C. Asbury and Craig A. Hunter
Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control / / Scott C. Asbury and Craig A. Hunter
Autore Asbury Scott C.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 1999
Descrizione fisica 1 online resource (134 pages) : illustrations
Collana NASA/TM
Soggetto topico Exhaust nozzles
Porosity
Hole geometry (mechanics)
Cavities
Thrust vector control
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706145403321
Asbury Scott C.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 1999
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Toward cooling uniformity : investigation of spiral, sweeping holes, and unconventional cooling paradigms / / Vikram Shyam [and four others]
Toward cooling uniformity : investigation of spiral, sweeping holes, and unconventional cooling paradigms / / Vikram Shyam [and four others]
Autore Shyam Vikram
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , March 2018
Descrizione fisica 1 online resource (32 pages) : color illustrations
Collana NASA/TM
Soggetto topico Thermocouples
Hole geometry (mechanics)
Thermography
Flow velocity
Film cooling
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Toward cooling uniformity
Record Nr. UNINA-9910706922703321
Shyam Vikram  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , March 2018
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui