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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Wing leading edge joint laminar flow tests / / Aaron Drake [and four others] |
Autore | Drake Aaron |
Pubbl/distr/stampa | Moffett Field, California, : National Aeronautics and Space Administration, Ames Research Center, October 1996 |
Descrizione fisica | 1 online resource (33 pages) : illustrations |
Collana | NASA technical memorandum |
Soggetto topico |
F-104 aircraft
Laminar flow airfoils Friction measurement Skin friction Pressure distribution |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910704205203321 |
Drake Aaron | ||
Moffett Field, California, : National Aeronautics and Space Administration, Ames Research Center, October 1996 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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