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Effects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan [[electronic resource] /] / Gregory P. Herrick ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010



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Autore: Herrick Gregory Paul <1972-> Visualizza persona
Titolo: Effects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan [[electronic resource] /] / Gregory P. Herrick ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010 Visualizza cluster
Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011]
Descrizione fisica: 1 online resource (14 pages) : color illustrations
Soggetto topico: Aeroelasticity
Turbomachinery
Turbofans
Computational fluid dynamics
Inlet flow
Aerodynamic characteristics
High speed
Note generali: Title from title screen (viewed on June 27, 2011).
"January 2011."
"AIAA-2010-6711."
Nota di bibliografia: Includes bibliographical references (pages 13-14).
Titolo autorizzato: Effects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan  Visualizza cluster
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910700302303321
Lo trovi qui: Univ. Federico II
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