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Record Nr. |
UNINA9910702682503321 |
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Autore |
Sanders Bobby W. |
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Titolo |
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 |
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Pubbl/distr/stampa |
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Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Office, , January 1980 |
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Descrizione fisica |
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1 online resource (iii, 98 pages) : illustrations |
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Collana |
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NASA technical paper ; ; 1531 |
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Soggetti |
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Airplanes - Turbojet engines - Air intakes |
Airplanes - Motors - Valves |
Aerodynamic stability |
Bypasses |
Propulsion system performance |
Supersonic inlets |
Turbojet engines |
Wind tunnel stability tests |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Title from title screen (viewed Sept. 22, 2014). |
"January 1980." |
"Performing organization, Lewis Research Center"--Technical report documentation page. |
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Nota di bibliografia |
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Includes bibliographical references (pages 27-28). |
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