Explore how engineers model transonic flow over swept wings with advanced numerical methods.
This book presents a rigorous approach to predicting inviscid, compressible flow using the full potential equation. It explains how a rotated finite-difference scheme, non-conservative in form, can be combined with coordinate transformations to capture flow details near the wing leading edge and along a vortex sheet.
This work frames the geometry, transformations, and numerical techniques needed to solve complex flow fields around swept configurations. It discusses the challenges of shocks, boundary layers, and the importance of preserving shock jumps, offering practical guidance on when conservation-form schemes are beneficial. The presentation is grounded in a clear sequence from physical space to computational domain, helping you understand how the method handles real-world wing shapes and attitudes."synopsis" may belong to another edition of this title.
Seller: PBShop.store US, Wood Dale, IL, U.S.A.
HRD. Condition: New. New Book. Shipped from UK. Established seller since 2000. Seller Inventory # LW-9780331554137
Seller: PBShop.store UK, Fairford, GLOS, United Kingdom
HRD. Condition: New. New Book. Shipped from UK. Established seller since 2000. Seller Inventory # LW-9780331554137
Quantity: 15 available