CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction / / David O. Davis

• Autore: Davis David O.
• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2015
• Descrizione fisica: 1 online resource (13 pages) : color illustrations
• Soggetto topico: Boundary layers; Computational fluid dynamics; Shock wave interaction; Flow measurement; Turbulent flow
• Note generali: Title from title screen (viewed on Feb. 2, 2016).; "September 2015."; "Prepared for the Joint Fluids Engineering Conference 2015 cosponsored by ASME, JSME, and KSME, Seoul, Korea, July 26-31, 2015
• Nota di bibliografia: Includes bibliographical references (page 13).
• Altri titoli varianti: Computational fluid dynamics validation experiment of a Mach 2.5 axisymmetric shock wave boundary layer interaction
• Titolo autorizzato: CFD validation experiment of a Mach 2.5 axisymmetric shock-wave
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910704277603321
• Lo trovi qui: Univ. Federico II