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Analysis of inlet-compressor acoustic interactions using coupled CFD codes / / A. Suresh [and four others]
| Analysis of inlet-compressor acoustic interactions using coupled CFD codes / / A. Suresh [and four others] |
| Autore | Suresh A (Writer on numeric analysis) |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1998 |
| Descrizione fisica | 1 online resource (10 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Turbomachinery Supersonic inlets Unsteady aerodynamics |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706195103321 |
Suresh A (Writer on numeric analysis)
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1998 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Axisymmetric calculations of a low-boom inlet in a supersonic wind tunnel / / Rodrick V. Chima and Stefanie M. Hirt, Robert Reger
| Axisymmetric calculations of a low-boom inlet in a supersonic wind tunnel / / Rodrick V. Chima and Stefanie M. Hirt, Robert Reger |
| Autore | Chima Rodrick V |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] |
| Descrizione fisica | 1 online resource (12 pages) : illustrations (chiefly color) |
| Altri autori (Persone) |
HirtStefanie M
RegerRobert |
| Collana | NASA/TM |
| Soggetto topico |
Supersonic inlets
Computational fluid dynamics Mass flow Flight paths Supersonic aircraft Stability |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701560503321 |
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Chima Rodrick V
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Computational analysis of a low-boom supersonic inlet / / Rodrick V. Chima
| Computational analysis of a low-boom supersonic inlet / / Rodrick V. Chima |
| Autore | Chima Rodrick V |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] |
| Descrizione fisica | 1 online resource (14 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Engine inlets Supersonic aircraft Supersonic inlets Inlet airframe configurations Overpressure Supersonic flow Sonic booms Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701537703321 |
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Chima Rodrick V
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Design and analysis tool for external-compression supersonic inlets / / John W. Slater
| Design and analysis tool for external-compression supersonic inlets / / John W. Slater |
| Autore | Slater John W |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (23 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Supersonic inlets Flow distribution Aerodynamic characteristics Drag Flow velocity Supersonic speed |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702353503321 |
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Slater John W
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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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 |
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Sanders Bobby W.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Office, , January 1980 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct / / Milo D. Dahl
| The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct / / Milo D. Dahl |
| Autore | Dahl Milo D. <1956-> |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , November 1996 |
| Descrizione fisica | 1 online resource (21 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Supersonic jet flow
Ducts Ducted flow Duct geometry Circles (geometry) Boundary conditions Kelvin-Helmholtz instability Supersonic inlets |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707311303321 |
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Dahl Milo D. <1956->
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , November 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack / / Eldon A. Latham
| Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack / / Eldon A. Latham |
| Autore | Latham Eldon A. |
| Pubbl/distr/stampa | Moffett Field, California : , : Ames Research Center, , May 1976 |
| Descrizione fisica | 1 online resource (79 pages) : illustrations |
| Collana | NASA TM |
| Soggetto topico |
Supersonic inlets
Aerodynamics Mach number Jet engines - Air intakes Airplanes - Air ducts Air ducts - Aerodynamics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716991003321 |
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Latham Eldon A.
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| Moffett Field, California : , : Ames Research Center, , May 1976 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Joint US / Russia TU-144 engine ground tests / / Waldo A. Acosta [and four others]
| Joint US / Russia TU-144 engine ground tests / / Waldo A. Acosta [and four others] |
| Autore | Acosta Waldo A. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center : , : U.S. Army Research Laboratory, , June 1997 |
| Descrizione fisica | 1 online resource (39 pages) : illustrations |
| Collana |
NASA TM
ARL-TR |
| Soggetto topico |
Aircraft engines
Engine tests Flow characteristics Supersonic inlets Supersonic transports TU-144 aircraft |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Joint United States Russia TU-144 engine ground tests |
| Record Nr. | UNINA-9910707633503321 |
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Acosta Waldo A.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center : , : U.S. Army Research Laboratory, , June 1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds / / Joseph W. Connolly and George Kopasakis ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010
| Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds / / Joseph W. Connolly and George Kopasakis ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010 |
| Autore | Connolly Joseph W |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
| Descrizione fisica | 1 online resource (19 pages) : illustrations (color) |
| Altri autori (Persone) | KopasakisGeorge |
| Collana | NASA/TM |
| Soggetto topico |
Supersonic flight
Control systems design Supersonic transports Specifications Supersonic inlets Dynamic models Loops Feedback control Supersonic wind tunnels Flow distribution Computational fluid dynamics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory |
| Record Nr. | UNINA-9910700358203321 |
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Connolly Joseph W
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Minimum weight design of a generic axisymmetric inlet / / Shari-Beth Nadell
| Minimum weight design of a generic axisymmetric inlet / / Shari-Beth Nadell |
| Autore | Nadell Shari-Beth |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , August 1996 |
| Descrizione fisica | 1 online resource (13 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Symmetry
Air intakes Finite element method Supersonic inlets Structural design Structural weight Engine design |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707178503321 |
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Nadell Shari-Beth
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , August 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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