Articoli correlati a Numerical Calculation of the Transonic Flow Past a...
Sinossi
Predict transonic flow over swept wings with a robust numerical method. This edition explains how the full potential equation is solved on complex wing geometries.
This book presents a practical approach to predicting inviscid, transonic flows around swept wings. It describes a finite-difference framework and a rotated difference scheme, focusing on how geometry and coordinate choices affect accuracy and stability in simulations.
- Learn how coordinate transformations and conformal mappings simplify boundary conditions on wing surfaces.
- Understand how nonconservative and conservative formulations influence shock behavior and modeling of shock-boundary layer interactions.
- See how vortex sheets and trailing-edge dynamics are represented in a numerical setting.
- Explore the setup of a rectangular computational domain and the handling of far-field and near-edge regions with stretching transformations.
Le informazioni nella sezione "Riassunto" possono far riferimento a edizioni diverse di questo titolo.
Risultati della ricerca per Numerical Calculation of the Transonic Flow Past a...
Immagini fornite dal venditore
Numerical Calculation of the Transonic Flow Past a Swept Wing (Classic Reprint)
Print on DemandDa: Forgotten Books, London, Regno Unito
Valutazione del venditore 5 su 5 stelle
Paperback. Condizione: New. Print on Demand. This book analyzes the transonic potential flow past a swept wing, extending the computational method of Jameson for an airfoil to the three-dimensional case. The flow is analyzed in coordinates nearly conformally mapped from the physical space in planes parallel to the symmetry plane, reducing the wing surface to a portion of one boundary of the computational grid. The finite difference approximation is in conservation form, which introduces substantial errors in the treatment of shocks without using a shock fitting scheme or else a difference scheme in conservation form. To assure the correct shock jump relations the author uses a rotated difference scheme, and the difference equations are solved by relaxation. The method is capable of treating wings of arbitrary planform and dihedral, although approximations in treating the tips and vortex sheet make its accuracy suspect for wings of small aspect ratio. This book is a reproduction of an important historical work, digitally reconstructed using state-of-the-art technology to preserve the original format. In rare cases, an imperfection in the original, such as a blemish or missing page, may be replicated in the book. print-on-demand item. Codice articolo 9781332956432_0
Compra nuovo
EUR 16,72
Spedizione gratuita
Spedito da Regno Unito a U.S.A.
Spedito da Regno Unito a U.S.A.
Quantità: Più di 20 disponibili
Foto dell'editore
Numerical Calculation of the Transonic Flow Past a Swept Wing (Classic Reprint)
Da: PBShop.store US, Wood Dale, IL, U.S.A.
Valutazione del venditore 5 su 5 stelle
PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000. Codice articolo LW-9781332956432
Compra nuovo
EUR 26,45
Spedizione gratuita
Spedito in U.S.A.
Spedito in U.S.A.
Quantità: 15 disponibili
Foto dell'editore
Numerical Calculation of the Transonic Flow Past a Swept Wing (Classic Reprint)
Da: PBShop.store UK, Fairford, GLOS, Regno Unito
Valutazione del venditore 5 su 5 stelle
PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000. Codice articolo LW-9781332956432
Compra nuovo
EUR 25,36
Spedizione EUR 3,84
Spedito da Regno Unito a U.S.A.
Spedito da Regno Unito a U.S.A.
Quantità: 15 disponibili
Foto dell'editore
Numerical Calculation of the Transonic Flow Past a Swept Wing (Classic Reprint)
Print on DemandDa: Revaluation Books, Exeter, Regno Unito
Valutazione del venditore 5 su 5 stelle
Paperback. Condizione: Brand New. 106 pages. 9.06x5.98x0.47 inches. This item is printed on demand. Codice articolo zk1332956432
Compra nuovo
EUR 20,51
Spedizione EUR 11,67
Spedito da Regno Unito a U.S.A.
Spedito da Regno Unito a U.S.A.
Quantità: 1 disponibili
Foto dell'editore
Numerical Calculation of the Transonic Flow Past a Swept Wing (Classic Reprint)
Da: Buchpark, Trebbin, Germania
Valutazione del venditore 5 su 5 stelle
Condizione: Sehr gut. Zustand: Sehr gut | Sprache: Englisch | Produktart: Bücher | Keine Beschreibung verfügbar. Codice articolo 26922228/2
Compra usato
EUR 8,98
Spedizione EUR 105,00
Spedito da Germania a U.S.A.
Spedito da Germania a U.S.A.
Quantità: 8 disponibili
Foto dell'editore
Numerical Calculation of the Transonic Flow Past a Swept Wing (Classic Reprint)
Da: Buchpark, Trebbin, Germania
Valutazione del venditore 5 su 5 stelle
Condizione: Hervorragend. Zustand: Hervorragend | Sprache: Englisch | Produktart: Bücher | Keine Beschreibung verfügbar. Codice articolo 26922228/1
Compra usato
EUR 10,21
Spedizione EUR 105,00
Spedito da Germania a U.S.A.
Spedito da Germania a U.S.A.
Quantità: 1 disponibili