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CFD analysis of nozzle jet plume effects on sonic boom signature [[electronic resource] /] / Trong T. Bui
CFD analysis of nozzle jet plume effects on sonic boom signature [[electronic resource] /] / Trong T. Bui
Autore Bui Trong T
Pubbl/distr/stampa Edwards, Calif. : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , [2009]
Descrizione fisica 1 online resource (40 pages) : illustrations (some color)
Altri autori (Persone) BuiTrong T
Collana NASA/TM
Soggetto topico Computational fluid dynamics
Nozzle flow
Gas jets
Nozzle geometry
Sonic booms
Wind tunnel tests
Plumes
F-15 aircraft
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Computational fluid dynamics analysis of nozzle jet plume effects on sonic boom signature
Record Nr. UNINA-9910696907403321
Bui Trong T  
Edwards, Calif. : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , [2009]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Exhaust nozzle plume effects on sonic boom test results for vectored nozzles [[electronic resource] /] / Raymond Castner
Exhaust nozzle plume effects on sonic boom test results for vectored nozzles [[electronic resource] /] / Raymond Castner
Autore Castner Raymond S
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Descrizione fisica 1 online resource (16 pages) : color illustrations
Collana NASA/TM
Soggetto topico Exhaust nozzles
Sonic booms
Computational fluid dynamics
Elastic waves
Plumes
F-15 aircraft
Supersonic aircraft
Pressure ratio
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910701950003321
Castner Raymond S  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane / / Frank J. Kurtenbach and Frank W. Burcham, Jr
Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane / / Frank J. Kurtenbach and Frank W. Burcham, Jr
Autore Kurtenbach Frank J.
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , January 1981
Descrizione fisica 1 online resource (18 pages) : illustrations
Collana NASA technical paper
Soggetto topico Afterburning
F-15 aircraft
Jet thrust
Pressure measurement
Turbofan engines
Airplanes - Motors - Thrust
Fighter planes - Turbojet engines
Jet propulsion
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707439203321
Kurtenbach Frank J.  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , January 1981
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Flight test results on the stability and control of the F-15 Quiet Spike aircraft / / Cheng M. Moua [and three others]
Flight test results on the stability and control of the F-15 Quiet Spike aircraft / / Cheng M. Moua [and three others]
Autore Moua Cheng M.
Pubbl/distr/stampa Edwards, CA : , : National Aeronautics and, Space Administration, Dryden Flight Research Center, , [2012]
Descrizione fisica 1 online resource (41 pages) : color illustrations
Collana [NASA technical memorandum]
Soggetto topico F-15 aircraft
Flight tests
Aircraft control
Aircraft stability
Supersonic flight
Sonic booms
Fuselages
Noses (forebodies)
Computational fluid dynamics
Flight control
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702345403321
Moua Cheng M.  
Edwards, CA : , : National Aeronautics and, Space Administration, Dryden Flight Research Center, , [2012]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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High stability engine control (HISTEC) flight test results / / Robert D. Southwick [and six others]
High stability engine control (HISTEC) flight test results / / Robert D. Southwick [and six others]
Autore Southwick Robert D.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1998
Descrizione fisica 1 online resource (9 pages) : color illustrations
Collana NASA/TM
Soggetto topico Engine control
F-15 aircraft
Flight tests
Aircraft engines
Flow distortion
Thrust control
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti High stability engine control
Record Nr. UNINA-9910705842803321
Southwick Robert D.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1998
Materiale a stampa
Lo trovi qui: Univ. Federico II
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The high stability engine control (HISTEC) program : flight demonstration phase / / John C. DeLaat [and three others]
The high stability engine control (HISTEC) program : flight demonstration phase / / John C. DeLaat [and three others]
Autore DeLaat John C.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1998
Descrizione fisica 1 online resource (11 pages) : color illustrations
Collana NASA/TM
Soggetto topico Engine control
Gas turbine engines
Flight tests
F-15 aircraft
Flow distortion
Real time operation
On-line systems
Control systems design
Inlet pressure
Stability augmentation
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti High stability engine control
Record Nr. UNINA-9910705842703321
DeLaat John C.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1998
Materiale a stampa
Lo trovi qui: Univ. Federico II
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In-flight boundary-layer transition on a large flat plate at supersonic speeds / / D.W. Banks [and four others]
In-flight boundary-layer transition on a large flat plate at supersonic speeds / / D.W. Banks [and four others]
Autore Banks D. W.
Pubbl/distr/stampa Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , 2012
Descrizione fisica 1 online resource (21 pages) : color illustrations
Collana NASA/TM
Soggetto topico Boundary layer transition
Flat plates
Pressure distribution
Supersonic speed
Flight tests
F-15 aircraft
Infrared imagery
Airborne equipment
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910704473003321
Banks D. W.  
Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , 2012
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Optimal cooperative control synthesis of active displays / / by Sanjay Garg and David K. Schmidt ; submitted to NASA Dryden Flight Research Facility, Ames Research Center
Optimal cooperative control synthesis of active displays / / by Sanjay Garg and David K. Schmidt ; submitted to NASA Dryden Flight Research Facility, Ames Research Center
Autore Garg Sanjay
Pubbl/distr/stampa Edwards, Calif. : , : NASA Dryden Flight Research Facility, Ames Research Center, , 22 October, 1985
Descrizione fisica 1 online resource (xiv, 145 pages) : illustrations
Collana NASA contractor report
Soggetto topico Control systems design
Display devices
F-15 aircraft
Optimal control
Spectral methods
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910704182403321
Garg Sanjay  
Edwards, Calif. : , : NASA Dryden Flight Research Facility, Ames Research Center, , 22 October, 1985
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Proposed flight research of a dual-bell rocket nozzle using the NASA F-15 airplane / / Daniel S. Jones and Trong T. Bui, Joseph H. Ruf
Proposed flight research of a dual-bell rocket nozzle using the NASA F-15 airplane / / Daniel S. Jones and Trong T. Bui, Joseph H. Ruf
Autore Jones Daniel S.
Pubbl/distr/stampa Edwards, CA : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , September 2013
Descrizione fisica 1 online resource (17 pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Altitude tests
F-15 aircraft
Flight tests
Flow distribution
Nozzle design
Nozzle geometry
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702416503321
Jones Daniel S.  
Edwards, CA : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , September 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Subsonic flight test evaluation of a propulsion system parameter estimation process for the F-100 engine / / John S. Orme and Glenn B. Gilyard
Subsonic flight test evaluation of a propulsion system parameter estimation process for the F-100 engine / / John S. Orme and Glenn B. Gilyard
Autore Orme John S.
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , November 1992
Descrizione fisica 1 online resource (24 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Adaptive control
Aircraft performance
F-15 aircraft
Kalman filters
Optimal control
Propulsion system performance
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707954203321
Orme John S.  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , November 1992
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui