top

  Info

  • Utilizzare la checkbox di selezione a fianco di ciascun documento per attivare le funzionalità di stampa, invio email, download nei formati disponibili del (i) record.

  Info

  • Utilizzare questo link per rimuovere la selezione effettuata.
Analysis of an electrohydraulic aircraft control-surface servo and comparison with test results / / by John W. Edwards
Analysis of an electrohydraulic aircraft control-surface servo and comparison with test results / / by John W. Edwards
Autore Edwards John W.
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, , August 1972
Descrizione fisica 1 online resource (72 pages) : illustrations
Collana NASA/TN
Soggetto topico Hydraulic equipment
Control
Airplanes - Hydraulic equipment - Mathematical models
Airplanes - Control systems - Mathematical models
Hydraulic servomechanisms - Mathematical models
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910716554403321
Edwards John W.  
Washington, D.C. : , : National Aeronautics and Space Administration, , August 1972
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
MAVRIC flutter model transonic limit cycle oscillation test / / John W. Edwards [and four others]
MAVRIC flutter model transonic limit cycle oscillation test / / John W. Edwards [and four others]
Autore Edwards John W.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2001
Descrizione fisica 1 online resource (15 pages) : illustrations
Collana NASA/TM
Soggetto topico Transonic flow
Flutter
Wind tunnel models
Wing tips
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Models for aeroelastic validation research involving computation flutter model transonic limit cycle oscillation test
Record Nr. UNINA-9910691728603321
Edwards John W.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2001
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method / / John W. Edwards
Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method / / John W. Edwards
Autore Edwards John W.
Pubbl/distr/stampa [Washington, DC] : , : [National Aeronautics and Space Administration], , [1996]
Descrizione fisica 1 online resource (16 pages) : illustrations
Collana NASA-TM
Soggetto topico Separated flow
Transonic flow
Transonic flutter
Transonic speed
Unsteady flow
Viscous flow
Computational fluid dynamics
Coupling
Airfoils
Mach number
Boundary layer separation
Airfoil oscillations
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705776803321
Edwards John W.  
[Washington, DC] : , : [National Aeronautics and Space Administration], , [1996]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui