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Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 / / Francis J. Capone, E. Ann Bare, Dorothy Arbiter
Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 / / Francis J. Capone, E. Ann Bare, Dorothy Arbiter
Autore Capone Francis J.
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986
Descrizione fisica 1 online resource (102 pages) : illustrations
Collana NASA/TP
Soggetto topico Fighter aircraft
Aerodynamic characteristics
Aerodynamic configurations
Supersonic aircraft
Computer programs
Supersonic fighter planes
Aerodynamics, Supersonic
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910709714203321
Capone Francis J.  
Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Aerodynamic parameters of an advanced fighter aircraft estimated from flight data [[electronic resource] ] : preliminary results / / Vladislav Klein, Kevin P. Breneman, Thomas P. Ratvasky
Aerodynamic parameters of an advanced fighter aircraft estimated from flight data [[electronic resource] ] : preliminary results / / Vladislav Klein, Kevin P. Breneman, Thomas P. Ratvasky
Autore Klein Vladislav
Pubbl/distr/stampa Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1989]
Descrizione fisica iv, 53 pages : digital, PDF file
Altri autori (Persone) BrenemanKevin P
RatvaskyThomas P
Collana NASA technical memorandum
Soggetto topico Fighter planes
Aerodynamic characteristics
Aircraft instruments
Aircraft maneuvers
Fighter aircraft
Flight tests
Mathematical models
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Aerodynamic parameters of an advanced fighter aircraft estimated from flight data
Record Nr. UNINA-9910698069803321
Klein Vladislav  
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1989]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Computer-automated opponent for manned air-to-air combat simulations / / Walter W. Hankins III
Computer-automated opponent for manned air-to-air combat simulations / / Walter W. Hankins III
Autore Hankins Walter W.
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , September 1979
Descrizione fisica 1 online resource (150 pages) : illustrations
Collana NASA technical paper
Soggetto topico Airplanes, Military
Combat - Data processing
Combat
Computerized simulation
Fighter aircraft
Aircraft models
Automatic control
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702683203321
Hankins Walter W.  
Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , September 1979
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Feasibility and benefits of laminar flow control on supersonic cruise airplanes [[electronic resource] /] / A.G. Powell, S. Agrawal, T. R. Lacey
Feasibility and benefits of laminar flow control on supersonic cruise airplanes [[electronic resource] /] / A.G. Powell, S. Agrawal, T. R. Lacey
Autore Powell A. G
Pubbl/distr/stampa Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1989]
Descrizione fisica 1 volume
Altri autori (Persone) AgrawalSudhir
LaceyT. R
Collana NASA contractor report
Soggetto topico Aerodynamic configurations
Boundary layer control
Boundary layer stability
Feasibility analysis
Fighter aircraft
Laminar boundary layer
Laminar flow
Supersonic aircraft
Supersonic cruise aircraft research
Supersonic transports
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910698995003321
Powell A. G  
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1989]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Lateral-directional eigenvector flying qualities guidelines for high performance aircraft / / John B. Davidson, Dominick Andrisani, II
Lateral-directional eigenvector flying qualities guidelines for high performance aircraft / / John B. Davidson, Dominick Andrisani, II
Autore Davidson John B.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1996
Descrizione fisica 1 online resource (56 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Eigenvectors
Fighter aircraft
Supersonic aircraft
Flight characteristics
Lateral stability
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707905203321
Davidson John B.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Pressure distribution for the wing of the YAV-8B airplane: with and without pylons / / Edwin J. Saltzman [and three others]
Pressure distribution for the wing of the YAV-8B airplane: with and without pylons / / Edwin J. Saltzman [and three others]
Autore Saltzman Edwin J.
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 Fighter aircraft
Flow characteristics
Pressure distribution
Pylons
Supercritical wings
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Pressure distribution for the wing of the YAV-8B airplane
Record Nr. UNINA-9910707954103321
Saltzman Edwin J.  
[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
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Propulsion and airframe aerodynamic interactions of supersonic V/STOL configurations, Phase I / / M.R. Mraz, P.E. Hiley
Propulsion and airframe aerodynamic interactions of supersonic V/STOL configurations, Phase I / / M.R. Mraz, P.E. Hiley
Autore Mraz M. R.
Pubbl/distr/stampa St. Louis, Missouri : , : McDonnell Aircraft Company
Descrizione fisica 1 online resource (xii, 132 pages) : illustrations
Collana NASA contractor report
Soggetto topico Aerodynamic interference
Airframes
Fighter aircraft
Propulsion system configurations
Short takeoff aircraft
Supersonic aircraft
Vertical takeoff aircraft
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Propulsion and airframe aerodynamic interactions of supersonic V STOL configurations, Phase I
Record Nr. UNINA-9910705490303321
Mraz M. R.  
St. Louis, Missouri : , : McDonnell Aircraft Company
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Pseudosteady-state analysis of nonlinear aircraft maneuvers / / John W. Young, Albert A. Schy, and Katherine G. Johnson
Pseudosteady-state analysis of nonlinear aircraft maneuvers / / John W. Young, Albert A. Schy, and Katherine G. Johnson
Autore Young John W (John Worth), <1934->
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980
Descrizione fisica 1 online resource (61 pages) : illustrations
Collana NASA technical paper
Soggetto topico Aerodynamic characteristics
Aircraft maneuvers
Angle of attack
Fighter aircraft
Flight characteristics
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707459203321
Young John W (John Worth), <1934->  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

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