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Design and evaluation of a new boundary layer rake for flight testing / / Trong T. Bui and David L. Oates, Jose c. Gonsalez
Design and evaluation of a new boundary layer rake for flight testing / / Trong T. Bui and David L. Oates, Jose c. Gonsalez
Autore Bui Trong T.
Pubbl/distr/stampa Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Reserch Center, , January 2000
Descrizione fisica 1 online resource (16 pages) : illustrations
Collana NASA/TM
Soggetto topico Boundary layers
Pressure sensors
Design analysis
Structural design
Flight test instruments
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706265103321
Bui Trong T.  
Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Reserch Center, , January 2000
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8 / / Mark C. Davis [and five others]
Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8 / / Mark C. Davis [and five others]
Autore Davis Mark C.
Pubbl/distr/stampa Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Reserch Center, , May 2000
Descrizione fisica 1 online resource (20 pages) : illustrations
Collana NASA TM
Soggetto topico Mach number
Research vehicles
Supersonic combustion ramjet engines
Wind tunnel tests
Air data systems
Design analysis
Detection
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706263503321
Davis Mark C.  
Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Reserch Center, , May 2000
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Experimental and numerical characterization of a steady-state cylindrical blackbody cavity at 1100 degrees celsius / / Thomas J. Horn, Amanie N. Abdelmessih
Experimental and numerical characterization of a steady-state cylindrical blackbody cavity at 1100 degrees celsius / / Thomas J. Horn, Amanie N. Abdelmessih
Autore Horn Thomas J.
Pubbl/distr/stampa Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Reserch Center, , August 2000
Descrizione fisica 1 online resource (15 pages) : illustrations
Collana NASA/TM
Soggetto topico Experimentation
Numerical analysis
Steady state
Cavities
Cylindrical bodies
Heat transfer
Measuring instruments
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706239903321
Horn Thomas J.  
Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Reserch Center, , August 2000
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Pegasus wing-glove experiment to document hypersonic crossflow transition : measurement systems and selected flight results / / Arild Bertelrud [and ten others]
Pegasus wing-glove experiment to document hypersonic crossflow transition : measurement systems and selected flight results / / Arild Bertelrud [and ten others]
Autore Bertelrud Arild
Pubbl/distr/stampa Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Reserch Center, , January 2000
Descrizione fisica 1 online resource (24 pages) : illustrations
Collana NASA/TM
Soggetto topico Aerodynamics, Hypersonic
Hypersonic flow
Measuring instruments
Flight characteristics
Cross flow
Pegasus air-launched booster
Boundary layer transition
Flight tests
Data acquisition
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Pegasus wing-glove experiment to document hypersonic crossflow transition
Record Nr. UNINA-9910706264203321
Bertelrud Arild  
Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Reserch Center, , January 2000
Materiale a stampa
Lo trovi qui: Univ. Federico II
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A real-time method for estimating viscous forebody drag coefficients / / Stephen A. Whitmore [and three others]
A real-time method for estimating viscous forebody drag coefficients / / Stephen A. Whitmore [and three others]
Autore Whitmore Stephen A.
Pubbl/distr/stampa Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Reserch Center, , January 2000
Descrizione fisica 1 online resource (28 pages) : illustrations
Collana NASA/TM
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706264803321
Whitmore Stephen A.  
Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Reserch Center, , January 2000
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui