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.
Analysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed [[electronic resource] /] / by Arthur F. Smith
| Analysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed [[electronic resource] /] / by Arthur F. Smith |
| Autore | Smith Arthur F |
| Pubbl/distr/stampa | Windsor Locks, Conn. : , : Hamilton Standard Division, United Technologies Corporation |
| Descrizione fisica | 1 online resource (x, 101/102 pages) : illustrations |
| Collana | NASA CR |
| Soggetto topico |
Aerodynamic stability
Dynamic response Dynamic structural analysis Evaluation Prop-fan technology Turboprop engines |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701902203321 |
Smith Arthur F
|
||
| Windsor Locks, Conn. : , : Hamilton Standard Division, United Technologies Corporation | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Calculated low-speed steady and time-dependent aerodynamic derivatives for some airfoils using a discrete vortex method / / Donald R. Riley
| Calculated low-speed steady and time-dependent aerodynamic derivatives for some airfoils using a discrete vortex method / / Donald R. Riley |
| Autore | Riley Donald R. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 2015 |
| Descrizione fisica | 1 online resource (61 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aerodynamic coefficients
Aerodynamic stability Airfoils Time dependence Vortices |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707196803321 |
|
Riley Donald R.
|
||
| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Critical evaluation of the unsteady aerodynamics approach to dynamic stability at high angles of attack : final report / / prepared by W.H. Hui
| Critical evaluation of the unsteady aerodynamics approach to dynamic stability at high angles of attack : final report / / prepared by W.H. Hui |
| Autore | Hui W. H. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : [National Aeronautics and Space Administration], , 1985 |
| Descrizione fisica | 1 online resource (approximately 48 pages) |
| Collana | [NASA contractor report] |
| Soggetto topico |
Aerofoils
Equations of motion Unsteady flow (Aerodynamics) Stability of airplanes Aerodynamic stability Airfoils Branching (mathematics) Hysteresis Oscillations Unsteady aerodynamics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Critical evaluation of the unsteady aerodynamics approach to dynamic stability at high angles of attack |
| Record Nr. | UNINA-9910715477503321 |
|
Hui W. H.
|
||
| [Washington, D.C.] : , : [National Aeronautics and Space Administration], , 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients / / Bobby W. Sanders
| Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients / / Bobby W. Sanders |
| Autore | Sanders Bobby W. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Office, , January 1980 |
| Descrizione fisica | 1 online resource (iii, 98 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Airplanes - Turbojet engines - Air intakes
Airplanes - Motors - Valves Aerodynamic stability Bypasses Propulsion system performance Supersonic inlets Turbojet engines Wind tunnel stability tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702682503321 |
|
Sanders Bobby W.
|
||
| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Office, , January 1980 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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 | ||
| ||
Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft / / W.G. Steenken [and three others]
| Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft / / W.G. Steenken [and three others] |
| Autore | Steenken William G. |
| Pubbl/distr/stampa | Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Research Center, February 1999 |
| Descrizione fisica | 1 online resource (vii, 191 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
F-18 aircraft
Aerodynamic stability Angle of attack Compressors Control surfaces Flight control Research vehicles Rotors Subsonic speed |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706189103321 |
|
Steenken William G.
|
||
| Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Research Center, February 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops / / Zachary T. Applin and Paul L. Coe, Jr
| Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops / / Zachary T. Applin and Paul L. Coe, Jr |
| Autore | Applin Zachary T. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 |
| Descrizione fisica | 1 online resource (iii, 63 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Aerodynamic stability
Aerodynamic characteristics Transport aircraft Propellers Control stability Turboprop transports Stability of airplanes |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709793703321 |
|
Applin Zachary T.
|
||
| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Multi-mission system analysis for planetary entry (M-SAPE) version 1 / / Jamshid Samareh [and thirteen others]
| Multi-mission system analysis for planetary entry (M-SAPE) version 1 / / Jamshid Samareh [and thirteen others] |
| Autore | Samareh Jamshid |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2014 |
| Descrizione fisica | 1 online resource (x, 124 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Sample return missions
Atmospheric entry Aerodynamic stability Systems analysis Systems integration Flight mechanics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Multi-mission system analysis for planetary entry |
| Record Nr. | UNINA-9910703588303321 |
|
Samareh Jamshid
|
||
| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Output measurement equations for flexible aircraft flight dynamics / / Jared A. Grauer, Matthew J. Boucher
| Output measurement equations for flexible aircraft flight dynamics / / Jared A. Grauer, Matthew J. Boucher |
| Autore | Grauer Jared A. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 2018 |
| Descrizione fisica | 1 online resource (31 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Flexible wings
Flight test instruments Aerodynamic stability Output Aircraft instruments |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910711660603321 |
|
Grauer Jared A.
|
||
| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 2018 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Potential benefits of magnetic suspension and balance systems [[electronic resource] /] / Pierce L. Lawing, David A. Dress, and Robert A. Kilgore
| Potential benefits of magnetic suspension and balance systems [[electronic resource] /] / Pierce L. Lawing, David A. Dress, and Robert A. Kilgore |
| Autore | Lawing Pierce L |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1987] |
| Descrizione fisica | 1 volume |
| Altri autori (Persone) |
DressDavid A
KilgoreRobert A |
| Collana | NASA technical memorandum |
| Soggetto topico |
Aerodynamic balance
Aerodynamic coefficients Aerodynamic stability Magnetic suspension Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910698894603321 |
|
Lawing Pierce L
|
||
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1987] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
