Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods / / Gregory P. Herrick

• Autore: Herrick Gregory Paul <1972->
• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2014
• Descrizione fisica: 1 online resource (17 pages) : color illustrations
• Soggetto topico: Turbomachinery; Flutter analysis; Inlet flow; Computational fluid dynamics; Aeroelasticity
• Note generali: Title from title screen (viewed on June 3, 2015).; "December 2014."; "Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 28-30, 2014."
• Nota di bibliografia: Includes bibliographical references (pages 15-17).
• Titolo autorizzato: Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910703769103321
• Lo trovi qui: Univ. Federico II