Computation of supersonic flow over flying configurations

This high-level aerospace reference book will be useful for undergraduate and graduate students of engineering, applied mathematics and physics. The author provides solutions for three-dimensional compressible Navier-Stokes layer subsonic and supersonic flows.* Computational work and experimental r...

Descripción completa

Detalles Bibliográficos
Autor principal: Nastase, Adriana (-)
Formato: Libro electrónico
Idioma:Inglés
Publicado: Amsterdam ; Boston : Elsevier 2008.
Edición:1st ed
Materias:
Ver en Biblioteca Universitat Ramon Llull:https://discovery.url.edu/permalink/34CSUC_URL/1im36ta/alma991009627543306719
Descripción
Sumario:This high-level aerospace reference book will be useful for undergraduate and graduate students of engineering, applied mathematics and physics. The author provides solutions for three-dimensional compressible Navier-Stokes layer subsonic and supersonic flows.* Computational work and experimental results show the real-world application of computational results* Easy computation and visualization of inviscid and viscous aerodynamic characteristics of flying configurations* Includes a fully optimized and integrated design for a proposed supersonic transport aircraft
Notas:Description based upon print version of record.
Descripción Física:1 online resource (425 p.)
Bibliografía:Includes bibliographical references and indexes.
ISBN:9781281144690
9786611144692
9780080556994