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The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor / / Richard F. Bozak, Christopher E. Hughes, James Buckley
The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor / / Richard F. Bozak, Christopher E. Hughes, James Buckley
Autore Bozak Richard F.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2013
Descrizione fisica 1 online resource (8 pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Acoustic properties
Aerodynamic noise
Blade tips
Oscillating flow
Pressure ratio
Turbofans
Rotors
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705296503321
Bozak Richard F.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating [[electronic resource] /] / Vikram Shyam, Ali Ameri
Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating [[electronic resource] /] / Vikram Shyam, Ali Ameri
Autore Shyam Vikram
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Descrizione fisica 1 online resource (8 pages) : illustrations (some color)
Altri autori (Persone) AmeriAli
Collana NASA/TM
Soggetto topico Computational fluid dynamics
Supersonic turbines
Blade tips
Supersonic flow
Rotor aerodynamics
Axial flow turbines
Supersonic heat transfer
Contours
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702216503321
Shyam Vikram  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight [[electronic resource] ] : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel / / Anthony Neal Watkins ... [and others]
Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight [[electronic resource] ] : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel / / Anthony Neal Watkins ... [and others]
Pubbl/distr/stampa Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011]
Descrizione fisica 1 online resource (18 pages) : color illustrations
Altri autori (Persone) WatkinsAnthony Neal
Collana NASA/TM
Soggetto topico Pressure measurement
Pressure sensitive paints
Flow distribution
Flight simulation
Pressure sensors
Horizontal flight
Blade tips
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight
Record Nr. UNINA-9910701779103321
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines [[electronic resource] /] / A.A. Ameri, E. Steinthorsson, David L. Rigby
Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines [[electronic resource] /] / A.A. Ameri, E. Steinthorsson, David L. Rigby
Autore Ameri Ali A
Pubbl/distr/stampa [Cleveland, Ohio] : , : National Aeronautics and Space Administration, Lewis Research Center, , [1998]
Descrizione fisica 1 online resource (12 pages) : illustrations
Altri autori (Persone) SteinthorssonErlendur
RigbyD. L <1963-> (David Lester)
Collana NASA/CR
Soggetto topico Gas turbines
Heat transfer
Axial flow turbines
Blade tips
Clearances
Recesses
Gas-turbines
Heat - Transmission
School recess breaks
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702063403321
Ameri Ali A  
[Cleveland, Ohio] : , : National Aeronautics and Space Administration, Lewis Research Center, , [1998]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Evaluation of an active clearance control system concept [[electronic resource] /] / Bruce M. Steinetz ... [and others] ; prepared for the 41st Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Tucson, Arizona, July 10-13, 2005
Evaluation of an active clearance control system concept [[electronic resource] /] / Bruce M. Steinetz ... [and others] ; prepared for the 41st Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Tucson, Arizona, July 10-13, 2005
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005]
Descrizione fisica 1 online resource (14 pages) : illustrations
Altri autori (Persone) SteinetzBruce M
Collana NASA TM-
Soggetto topico Active control
Blade tips
Clearances
High pressure
Turbine blades
Turbines
Seals (stoppers)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910697003103321
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Heat transfer and flow on the first stage blade tip of a power generation gas turbine . Part 2 Simulation results [[electronic resource] /] / A.A. Ameri, R.S. Bunker
Heat transfer and flow on the first stage blade tip of a power generation gas turbine . Part 2 Simulation results [[electronic resource] /] / A.A. Ameri, R.S. Bunker
Autore Ameri Ali A
Pubbl/distr/stampa [Cleveland, Ohio] : , : National Aeronautics and Space Administration, Glenn Research Center
Altri autori (Persone) BunkerRonald S
Collana [NASA contractor report]
Soggetto topico Gas turbines
Heat transfer
Mathematical models
Blade tips
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Simulation results
Record Nr. UNINA-9910692113903321
Ameri Ali A  
[Cleveland, Ohio] : , : National Aeronautics and Space Administration, Glenn Research Center
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Helicopter blade tips [[electronic resource] /] / R. Lyothier
Helicopter blade tips [[electronic resource] /] / R. Lyothier
Autore Lyothier R
Pubbl/distr/stampa Santa Barbara, CA : , : Scitran
Descrizione fisica 1 online resource (ii, 26 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Blade tips
Helicopter design
Helicopter performance
Supersonic flutter
Vortex alleviation
Wing tip vortices
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702106903321
Lyothier R  
Santa Barbara, CA : , : Scitran
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Integrated turbine tip clearance and gas turbine engine simulation / / Jeffryes W. Chapman [and three others]
Integrated turbine tip clearance and gas turbine engine simulation / / Jeffryes W. Chapman [and three others]
Autore Chapman Jeffryes W.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2016
Descrizione fisica 1 online resource (17 pages) : color illustrations
Collana NASA/TM
Soggetto topico Blade tips
Gas turbine engines
Thermodynamics
Turbine blades
Turbocompressors
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707929203321
Chapman Jeffryes W.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Investigation of a Moiré based crack detection technique for propulsion health monitoring [[electronic resource] /] / Mark R. Woike ... [and others]
Investigation of a Moiré based crack detection technique for propulsion health monitoring [[electronic resource] /] / Mark R. Woike ... [and others]
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Descrizione fisica 1 online resource (12 pages) : illustrations (some color)
Altri autori (Persone) WoikeMark R
Collana NASA/TM
Soggetto topico Gas turbine engines
Blade tips
Clearances
Shafts (machine elements)
Cracks
Detection
Optical measurement
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702215303321
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984 [[electronic resource] /] / D. Parzych, [S. Cohen, A. Shenkman]
Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984 [[electronic resource] /] / D. Parzych, [S. Cohen, A. Shenkman]
Autore Parzych David J
Pubbl/distr/stampa [Washington, DC] : , : [National Aeronautics and Space Administration]
Descrizione fisica iv, 56 pages : illustrations
Altri autori (Persone) CohenS
ShenkmanArieh L
Collana NASA contractor report
Soggetto topico Aerodynamic characteristics
Aerodynamic noise
Acoustic properties
Blade tips
High speed
Mach number
Prop-fan technology
Propeller fans
Power efficiency
Weight (mass)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Large-scale Advanced Propfan
Record Nr. UNINA-9910700283803321
Parzych David J  
[Washington, DC] : , : [National Aeronautics and Space Administration]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

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