Chattot J J (16 results)

Hardcover. Condition: Brand New. 186 pages. 9.25x6.25x0.75 inches. In Stock.

Condition: New. In English.

Taschenbuch. Condition: Neu. Theoretical and Applied Aerodynamics | and Related Numerical Methods | J. J. Chattot (u. a.) | Taschenbuch | xxi | Englisch | 2016 | Springer | EAN 9789401777933 | Verantwortliche Person für die EU: Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, juergen[dot]hartmann[at]springer[dot]com | Anbieter: preigu. …

Condition: New. pp. 620.

Paperback. Condition: Like New. LIKE NEW. SHIPS FROM MULTIPLE LOCATIONS. book.

Condition: New. pp. 620.

Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Attractive from an educational view point by using potential flow models and viscous correctionsProvides a great balance between theory and numericsFocuses on aircrafts and theories that help estimating the forces and moments acting on them.…

Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Attractive from an educational view point by using potential flow models and viscous correctionsProvides a great balance between theory and numericsFocuses on aircrafts and theories that help estimating the forces and moments acting on them.…

Taschenbuch. Condition: Neu. This item is printed on demand - Print on Demand Titel. Neuware -This book covers classical and modern aerodynamics, theories and related numerical methods, for senior and first-year graduate engineering students, including:The classical potential (incompressible) flow theories for low speed aerodynamics of thin airfoils and high and low aspect ratio wings. The linearized theories for compressible subsonic and supersonic aerodynamics. The nonlinear transonic small disturbance potential flow theory, including supercritical wing sections, the extended transonic area rule with lift effect, transonic lifting line and swept or oblique wings to minimize wave drag. Unsteady flow is also briefly discussed. Numerical simulations based on relaxation mixed-finite difference methods are presented and explained. Boundary layer theory for all Mach number regimes and viscous/inviscid interaction procedures used in practical aerodynamics calculations.There are also four chapters covering special topics, including wind turbines and propellers, airplane design, flow analogies and hypersonic (rotational) flows.A unique feature of the book is its ten self-tests and their solutions as well as an appendix on special techniques of functions of complex variables, method of characteristics and conservation laws and shock waves. The book is the culmination of two courses taught every year by the two authors for the last two decades to seniors and first-year graduate students of aerospace engineering at UC Davis.Springer-Verlag KG, Sachsenplatz 4-6, 1201 Wien 644 pp. Englisch.…

Condition: new. Questo è un articolo print on demand.

Condition: New. Print on Demand pp. 620.

Condition: new. Questo è un articolo print on demand.

Buch. Condition: Neu. This item is printed on demand - Print on Demand Titel. Neuware -This book covers classical and modern aerodynamics, theories and related numerical methods, for senior and first-year graduate engineering students, including:The classical potential (incompressible) flow theories for low speed aerodynamics of thin airfoils and high and low aspect ratio wings. The linearized theories for compressible subsonic and supersonic aerodynamics. The nonlinear transonic small disturbance potential flow theory, including supercritical wing sections, the extended transonic area rule with lift effect, transonic lifting line and swept or oblique wings to minimize wave drag. Unsteady flow is also briefly discussed. Numerical simulations based on relaxation mixed-finite difference methods are presented and explained. Boundary layer theory for all Mach number regimes and viscous/inviscid interaction procedures used in practical aerodynamics calculations.There are also four chapters covering special topics, including wind turbines and propellers, airplane design, flow analogies and hypersonic (rotational) flows.A unique feature of the book is its ten self-tests and their solutions as well as an appendix on special techniques of functions of complex variables, method of characteristics and conservation laws and shock waves. The book is the culmination of two courses taught every year by the two authors for the last two decades to seniors and first-year graduate students of aerospace engineering at UC Davis.Springer-Verlag KG, Sachsenplatz 4-6, 1201 Wien 644 pp. Englisch.…

Condition: New. PRINT ON DEMAND pp. 620.

Condition: New. Print on Demand pp. 620.

Condition: New. PRINT ON DEMAND pp. 620.