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Measured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet [[electronic resource] /] / Domenic J. Maglieri and Herbert R. Henderson, Ana F. Tinetti
Measured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet [[electronic resource] /] / Domenic J. Maglieri and Herbert R. Henderson, Ana F. Tinetti
Autore Maglieri Domenic J
Pubbl/distr/stampa Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011]
Descrizione fisica 1 online resource (65 pages) : illustrations
Altri autori (Persone) HendersonHerbert R
TinettiAna Fiorella <1962->
Collana NASA/CR
Soggetto topico F-104 aircraft
Flow distribution
Sonic booms
Supersonic speed
B-70 aircraft
Shock waves
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910700818203321
Maglieri Domenic J  
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Measurements of a single lateral jet injected into swirling crossflow / / L.H. Ong and D.G. Lilley
Measurements of a single lateral jet injected into swirling crossflow / / L.H. Ong and D.G. Lilley
Autore Ong L. H.
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, , January 1986
Descrizione fisica 1 online resource (iii, 87 pages) : illustrations
Collana NASA/CR
Soggetto topico Lateral control
Turbulent flow
Flow distribution
Cross flow
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910709868203321
Ong L. H.  
Washington, D.C. : , : National Aeronautics and Space Administration, , January 1986
Materiale a stampa
Lo trovi qui: Univ. Federico II
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A method for data base management and analysis for wind-tunnel data [[electronic resource] /] / Aileen O. Biser
A method for data base management and analysis for wind-tunnel data [[electronic resource] /] / Aileen O. Biser
Autore Biser Aileen O
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , 1987
Descrizione fisica 1 volume
Collana NASA technical memorandum
Soggetto topico Data base management systems
Data processing
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910698898403321
Biser Aileen O  
Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , 1987
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Mid-fidelity computational fluid dynamics analysis of the Elytron 4S UAV concept / / Witold J. F. Koning [and three others]
Mid-fidelity computational fluid dynamics analysis of the Elytron 4S UAV concept / / Witold J. F. Koning [and three others]
Autore Koning Witold J. F.
Pubbl/distr/stampa Moffett Field, CA : , : National Aeronautics and Space Administration, Ames Research Center, , November 2018
Descrizione fisica 1 online resource (viii, 32 pages) : color illustrations
Collana NASA/TM
Soggetto topico Angle of attack
Directional stability
Rotary wing aircraft
Computational fluid dynamics
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910711770003321
Koning Witold J. F.  
Moffett Field, CA : , : National Aeronautics and Space Administration, Ames Research Center, , November 2018
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Modifications to the 4 x 7 meter tunnel for acoustic research [[electronic resource] ] : engineering feasibility study
Modifications to the 4 x 7 meter tunnel for acoustic research [[electronic resource] ] : engineering feasibility study
Pubbl/distr/stampa Orlando, Fla. : , : DSMA Engineering Corporation
Descrizione fisica 1 online resource (vii, 77 pages) : illustrations
Collana NASA contractor report
Soggetto topico Acoustic measurement
Aeroacoustics
Design analysis
Low speed wind tunnels
Wind tunnel drives
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Modifications to the 4 x 7 meter tunnel for acoustic research
Record Nr. UNINA-9910702107703321
Orlando, Fla. : , : DSMA Engineering Corporation
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds / / Robert J. Mack
Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds / / Robert J. Mack
Autore Mack Robert J.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999
Descrizione fisica 1 online resource (15 pages) : illustrations
Collana NASA/TM
Soggetto topico Aerodynamic characteristics
Body-wing configurations
Nacelles
Sonic booms
Wings
Aerodynamic configurations
Supersonic flight
Aerodynamic noise
Noise reduction
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706143703321
Mack Robert J.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle [[electronic resource] /] / Milton Lamb, William K. Abeyounis, and James C. Patterson, Jr
Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle [[electronic resource] /] / Milton Lamb, William K. Abeyounis, and James C. Patterson, Jr
Autore Lamb Milton
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , 1985
Descrizione fisica 1 online resource (58 pages) : illustrations
Altri autori (Persone) AbeyounisWilliam Kelly
PattersonJames C. <1942->
Collana NASA technical paper
Soggetto topico Laminar flow
Pylons
Transport aircraft
Turbulent flow
Wind tunnel tests
Wing nacelle configurations
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910701479303321
Lamb Milton  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , 1985
Materiale a stampa
Lo trovi qui: Univ. Federico II
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NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6 / / Stephen W.D. Wolf, James A. Laub
NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6 / / Stephen W.D. Wolf, James A. Laub
Autore Wolf Stephen W. D.
Pubbl/distr/stampa Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , March 1997
Descrizione fisica 1 online resource (iii, 21 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Laminar flow
Supersonic wind tunnels
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti NASA Ames Laminar Flow Supersonic Wind Tunnel
Record Nr. UNINA-9910708660203321
Wolf Stephen W. D.  
Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , March 1997
Materiale a stampa
Lo trovi qui: Univ. Federico II
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On hammershock propagation in a supersonic flow field / / A. Robert Porro
On hammershock propagation in a supersonic flow field / / A. Robert Porro
Autore Porro A. Robert
Pubbl/distr/stampa Cleveland Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2002
Descrizione fisica 1 online resource (9 pages) : illustrations
Collana NASA/TM
Soggetto topico Flight simulation
Flow distribution
-85 engine
Jet propulsion
Rotating stalls
Static pressure
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705686403321
Porro A. Robert  
Cleveland Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2002
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Orion Multi-Purpose Crew Vehicle (MPCV) Capsule Parachute Assembly System (CPAS) wake deficit wind tunnel testing / / James C. Ross, David M. Schuster
Orion Multi-Purpose Crew Vehicle (MPCV) Capsule Parachute Assembly System (CPAS) wake deficit wind tunnel testing / / James C. Ross, David M. Schuster
Autore Ross James C (James Carl), <1955->
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , February 2014
Descrizione fisica 1 online resource (86 pages) : color illustrations
Collana NASA/TM
Soggetto topico Wind tunnel tests
Drag chutes
Towed bodies
Spacecraft modules
Crew Exploration Vehicle
Velocity measurement
Parachutes
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Orion Multi-Purpose Crew Vehicle
Record Nr. UNINA-9910702659503321
Ross James C (James Carl), <1955->  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , February 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
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