Decambering: A numerical tool to predict post-stall aerodynamic data: Prediction of post-stall aerodynamic data for single and multiple wing configurations using airfoil data as input - Brossura
Sinossi
A novel scheme is presented for an iterative decambering approach to predict the post-stall characteristics of wings using known section data as inputs. The new scheme differs from earlier ones in the details of how the residual in the Newton iteration is computed. With earlier schemes, multiple solutions are obtained for wings at high angles of attack as the final converged solution depends on the initial conditions used for the iteration. With this scheme, multiple solutions at high angles of attack are brought to light right during the computation of the residuals for the Newton iteration. In general, the new scheme is found to be more robust at achieving convergence. Experimental validation is provided using experimental airfoil lift curves from Naik and Ostowari for three different aspect ratios of rectangular wings. Results are presented from a study of the stall characteristics of wings of different planform shapes and two configurations of a wing-tail and a wing-canard configuration. Results are also presented from a study to investigate possible asymmetric lift distributions when the iterations were started with an initial asymmetric distribution of the decambering.
Le informazioni nella sezione "Riassunto" possono far riferimento a edizioni diverse di questo titolo.
L'autore
Rinku Mukherjee is an Assistant Professor in Applied Mechanics at IIT, Madras, India. Her academic profile includes BE (Civil Engg., Jadavpur University, 1998), MS (Ocean Engg. and Naval Architecture, IITKgp, 2001) and PhD (Aerospace Engg., NCSU, 2004). Her current research interests are in formation flight and unsteady and post-stall aerodynamics.
Le informazioni nella sezione "Su questo libro" possono far riferimento a edizioni diverse di questo titolo.
Risultati della ricerca per Decambering: A numerical tool to predict post-stall...
Immagini fornite dal venditore
Decambering: A numerical tool to predict post-stall aerodynamic data
Editore:
LAP LAMBERT Academic Publishing Jun 2009, 2009
ISBN 10: 3838302095
ISBN 13: 9783838302096
Nuovo
Taschenbuch
Da: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germania
Valutazione del venditore 5 su 5 stelle
Taschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -A novel scheme is presented for an iterative decambering approach to predict the post-stall characteristics of wings using known section data as inputs. The new scheme differs from earlier ones in the details of how the residual in the Newton iteration is computed. With earlier schemes, multiple solutions are obtained for wings at high angles of attack as the final converged solution depends on the initial conditions used for the iteration. With this scheme, multiple solutions at high angles of attack are brought to light right during the computation of the residuals for the Newton iteration. In general, the new scheme is found to be more robust at achieving convergence. Experimental validation is provided using experimental airfoil lift curves from Naik and Ostowari for three different aspect ratios of rectangular wings. Results are presented from a study of the stall characteristics of wings of different planform shapes and two configurations of a wing-tail and a wing-canard configuration. Results are also presented from a study to investigate possible asymmetric lift distributions when the iterations were started with an initial asymmetric distribution of the decambering. 108 pp. Englisch. Codice articolo 9783838302096
Compra nuovo
EUR 49,00
Spese di spedizione:
EUR 23,00
Da: Germania a: U.S.A.
Quantità: 2 disponibili
Immagini fornite dal venditore
Decambering: A numerical tool to predict post-stallaerodynamic data
Editore:
LAP Lambert Academic Publishing, 2009
ISBN 10: 3838302095
ISBN 13: 9783838302096
Nuovo
Brossura
Da: moluna, Greven, Germania
Valutazione del venditore 4 su 5 stelle
Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. A novel scheme is presented for an iterative decambering approach to predict the post-stall characteristics of wings using known section data as inputs. The new scheme differs from earlier ones in the details of how the residual in the Newton iteration is c. Codice articolo 5410949
Compra nuovo
EUR 41,05
Spese di spedizione:
EUR 48,99
Da: Germania a: U.S.A.
Quantità: Più di 20 disponibili
Immagini fornite dal venditore
Decambering: A numerical tool to predict post-stall aerodynamic data
Editore:
LAP LAMBERT Academic Publishing Jun 2009, 2009
ISBN 10: 3838302095
ISBN 13: 9783838302096
Nuovo
Taschenbuch
Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germania
Valutazione del venditore 5 su 5 stelle
Taschenbuch. Condizione: Neu. Neuware -A novel scheme is presented for an iterative decambering approach to predict the post-stall characteristics of wings using known section data as inputs. The new scheme differs from earlier ones in the details of how the residual in the Newton iteration is computed. With earlier schemes, multiple solutions are obtained for wings at high angles of attack as the final converged solution depends on the initial conditions used for the iteration. With this scheme, multiple solutions at high angles of attack are brought to light right during the computation of the residuals for the Newton iteration. In general, the new scheme is found to be more robust at achieving convergence. Experimental validation is provided using experimental airfoil lift curves from Naik and Ostowari for three different aspect ratios of rectangular wings. Results are presented from a study of the stall characteristics of wings of different planform shapes and two configurations of a wing-tail and a wing-canard configuration. Results are also presented from a study to investigate possible asymmetric lift distributions when the iterations were started with an initial asymmetric distribution of the decambering.Books on Demand GmbH, Überseering 33, 22297 Hamburg 108 pp. Englisch. Codice articolo 9783838302096
Compra nuovo
EUR 49,00
Spese di spedizione:
EUR 60,00
Da: Germania a: U.S.A.
Quantità: 2 disponibili
Immagini fornite dal venditore
Decambering: A numerical tool to predict post-stall aerodynamic data : Prediction of post-stall aerodynamic data for single and multiple wing configurations using airfoil data as input
Editore:
LAP LAMBERT Academic Publishing, 2009
ISBN 10: 3838302095
ISBN 13: 9783838302096
Nuovo
Taschenbuch
Da: AHA-BUCH GmbH, Einbeck, Germania
Valutazione del venditore 5 su 5 stelle
Taschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - A novel scheme is presented for an iterative decambering approach to predict the post-stall characteristics of wings using known section data as inputs. The new scheme differs from earlier ones in the details of how the residual in the Newton iteration is computed. With earlier schemes, multiple solutions are obtained for wings at high angles of attack as the final converged solution depends on the initial conditions used for the iteration. With this scheme, multiple solutions at high angles of attack are brought to light right during the computation of the residuals for the Newton iteration. In general, the new scheme is found to be more robust at achieving convergence. Experimental validation is provided using experimental airfoil lift curves from Naik and Ostowari for three different aspect ratios of rectangular wings. Results are presented from a study of the stall characteristics of wings of different planform shapes and two configurations of a wing-tail and a wing-canard configuration. Results are also presented from a study to investigate possible asymmetric lift distributions when the iterations were started with an initial asymmetric distribution of the decambering. Codice articolo 9783838302096
Compra nuovo
EUR 49,00
Spese di spedizione:
EUR 60,90
Da: Germania a: U.S.A.
Quantità: 1 disponibili
Immagini fornite dal venditore
Decambering: A numerical tool to predict post-stall aerodynamic data | Prediction of post-stall aerodynamic data for single and multiple wing configurations using airfoil data as input
Editore:
LAP LAMBERT Academic Publishing, 2009
ISBN 10: 3838302095
ISBN 13: 9783838302096
Nuovo
Taschenbuch
Da: preigu, Osnabrück, Germania
Valutazione del venditore 5 su 5 stelle
Taschenbuch. Condizione: Neu. Decambering: A numerical tool to predict post-stall aerodynamic data | Prediction of post-stall aerodynamic data for single and multiple wing configurations using airfoil data as input | Rinku Mukherjee | Taschenbuch | 108 S. | Englisch | 2009 | LAP LAMBERT Academic Publishing | EAN 9783838302096 | Verantwortliche Person für die EU: BoD - Books on Demand, In de Tarpen 42, 22848 Norderstedt, info[at]bod[dot]de | Anbieter: preigu. Codice articolo 101548794
Compra nuovo
EUR 43,35
Spese di spedizione:
EUR 70,00
Da: Germania a: U.S.A.
Quantità: 5 disponibili