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Analysis of aerodynamic coefficients using gust gradient data: spanwise turbulence effects on airplane response / / Erik A. Ringnes and Walter Frost
Analysis of aerodynamic coefficients using gust gradient data: spanwise turbulence effects on airplane response / / Erik A. Ringnes and Walter Frost
Autore Ringnes Erik A.
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , February 1986
Descrizione fisica 1 online resource (x, 58 pages) : illustrations
Collana NASA/CR
Soggetto topico Aerodynamic forces
Stability derivatives
Turbulence
Airspeed
Flight safety
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Analysis of aerodynamic coefficients using gust gradient data
Record Nr. UNINA-9910709738203321
Ringnes Erik A.  
Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , February 1986
Materiale a stampa
Lo trovi qui: Univ. Federico II
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A comparison of three random number generators for aircraft dynamic modeling applications / / Jared A. Grauer
A comparison of three random number generators for aircraft dynamic modeling applications / / Jared A. Grauer
Autore Grauer Jared A.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2017
Descrizione fisica 1 online resource (37 pages) : illustrations
Collana NASA/TM
Soggetto topico Dynamic models
Fourier series
Monte Carlo method
Random numbers
Stability derivatives
White noise
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705714403321
Grauer Jared A.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2017
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Extraction of stability and control derivatives from orbiter flight data / / Kenneth W. Iliff and Mary F. Shafer
Extraction of stability and control derivatives from orbiter flight data / / Kenneth W. Iliff and Mary F. Shafer
Autore Iliff Kenneth W.
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , June 1993
Descrizione fisica 1 online resource (46 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Aerodynamic stability
Flight envelopes
Hypersonic flight
Space Shuttle orbiters
Stability derivatives
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705736603321
Iliff Kenneth W.  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , June 1993
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Important factors in the maximum likelihood analysis of flight test maneuvers / / Kenneth W. Iliff, Richard E. Maine, and T.D. Montgomery
Important factors in the maximum likelihood analysis of flight test maneuvers / / Kenneth W. Iliff, Richard E. Maine, and T.D. Montgomery
Autore Iliff Kenneth W.
Pubbl/distr/stampa [Washington, D.C.], : National Aeronautics and Space Administration, Scientific and Technical Information Office, April 1979
Descrizione fisica 1 online resource (iii, 40 pages) : illustrations
Collana NASA technical paper
Soggetto topico Aircraft performance
Dynamic tests
Flight control
Maximum likelihood estimates
Stability derivatives
Airplanes - Control systems
Airplanes - Flight testing
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707491403321
Iliff Kenneth W.  
[Washington, D.C.], : National Aeronautics and Space Administration, Scientific and Technical Information Office, April 1979
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Theory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow / / by M.J. Queijo
Theory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow / / by M.J. Queijo
Autore Queijo M. J.
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, , December 1968
Descrizione fisica 1 online resource (76 pages) : illustrations
Collana NASA/TN
Soggetto topico Compressible flow
Stability derivatives
Airplanes - Wings - Aerodynamics
Rolling (Aerodynamics)
Yawing (Aerodynamics)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910715901503321
Queijo M. J.  
Washington, D.C. : , : National Aeronautics and Space Administration, , December 1968
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui