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Decambering: A Numerical Tool to Predict Post-Stall Aerodynamic Data - rinku mukherjee
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rinku mukherjee:
Decambering: A Numerical Tool to Predict Post-Stall Aerodynamic Data - Taschenbuch

ISBN: 3838302095

ID: 10797703560

[EAN: 9783838302096], Neubuch, [PU: LAP Lambert Academic Publishing], RINKU MUKHERJEE,AERONAUTICS AND ASTRONAUTICS, Paperback. 108 pages. Dimensions: 8.7in. x 5.9in. x 0.2in.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. This item ships from multiple locations. Your book may arrive from Roseburg,OR, La Vergne,TN.

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Decambering: A Numerical Tool to Predict Post-Stall Aerodynamic Data (Paperback) - rinku mukherjee
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Decambering: A Numerical Tool to Predict Post-Stall Aerodynamic Data (Paperback) - Taschenbuch

2010, ISBN: 3838302095

ID: 18038031059

[EAN: 9783838302096], Neubuch, [PU: LAP Lambert Academic Publishing, Germany], Language: English Brand New Book ***** Print on Demand *****.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.

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Decambering: A numerical tool to predict post-stall aerodynamic data - Rinku Mukherjee
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ISBN: 9783838302096

ID: e924cdbb30b45f6479b2aba47d0c0803

A novel scheme is presented for an iterativedecambering approach to predict the post-stallcharacteristics of wings using known section data asinputs. The new scheme differs from earlier ones inthe details of how the residual in the Newtoniteration is computed. With earlier schemes, multiplesolutions are obtained forwings at high angles of attack as the final convergedsolution depends on theinitial conditions used for the iteration. With thisscheme, multiple solutions at high angles of attackare brought to light right during the computation ofthe residuals for the Newton iteration. In general,the new scheme is found to be more robust atachieving convergence. Experimental validation isprovided using experimental airfoil lift curves fromNaik and Ostowari for three different aspect ratiosof rectangular wings. Results are presented from astudy of the stall characteristics of wings ofdifferent planform shapes and two configurationsof a wing-tail and a wing-canard configuration.Results are also presented from a study toinvestigate possible asymmetric lift distributionswhen the iterations were started with an initialasymmetric distribution of the decambering. Bücher / Naturwissenschaften, Medizin, Informatik & Technik / Technik

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Decambering: A numerical tool to predict post-stallaerodynamic data - rinku mukherjee
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rinku mukherjee:
Decambering: A numerical tool to predict post-stallaerodynamic data - Taschenbuch

ISBN: 9783838302096

ID: 9783838302096

Prediction of post-stall aerodynamic data for singleand multiple wing configurations using airfoil dataas input A novel scheme is presented for an iterative Decambering: A numerical tool to predict post-stallaerodynamic data: A novel scheme is presented for an iterative, LAP Lambert Acad. Publ.

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Decambering: A numerical tool to predict post-stall aerodynamic data - Rinku Mukherjee
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Decambering: A numerical tool to predict post-stall aerodynamic data - neues Buch

ISBN: 9783838302096

ID: e924cdbb30b45f6479b2aba47d0c0803

A novel scheme is presented for an iterative

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Detailangaben zum Buch - Decambering: A numerical tool to predict post-stallaerodynamic data


EAN (ISBN-13): 9783838302096
ISBN (ISBN-10): 3838302095
Gebundene Ausgabe
Taschenbuch
Erscheinungsjahr: 2009
Herausgeber: LAP Lambert Acad. Publ.
108 Seiten
Gewicht: 0,181 kg
Sprache: eng/Englisch

Buch in der Datenbank seit 06.02.2008 21:31:35
Buch zuletzt gefunden am 20.09.2017 23:40:12
ISBN/EAN: 3838302095

ISBN - alternative Schreibweisen:
3-8383-0209-5, 978-3-8383-0209-6


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