Articoli correlati a Optimization of A Simple Aircraft Wing
- EditoreLAP LAMBERT Academic Publishing
- Data di pubblicazione2019
- ISBN 10 6139458048
- ISBN 13 9786139458042
- RilegaturaCopertina flessibile
- LinguaInglese
- Numero di pagine72
- Contatto del produttorenon disponibile
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Optimization of A Simple Aircraft Wing
Editore:
LAP LAMBERT Academic Publishing, 2019
ISBN 10: 6139458048
ISBN 13: 9786139458042
Antico o usato
Brossura
Da: Buchpark, Trebbin, Germania
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Condizione: Sehr gut. Zustand: Sehr gut | Seiten: 72 | Sprache: Englisch | Produktart: Bücher. Codice articolo 34239028/2
Quantità: 2 disponibili
Foto dell'editore
Optimization of A Simple Aircraft Wing
Editore:
LAP LAMBERT Academic Publishing, 2019
ISBN 10: 6139458048
ISBN 13: 9786139458042
Antico o usato
Brossura
Da: Buchpark, Trebbin, Germania
Valutazione del venditore 5 su 5 stelle
Condizione: Hervorragend. Zustand: Hervorragend | Seiten: 72 | Sprache: Englisch | Produktart: Bücher. Codice articolo 34239028/1
Quantità: 1 disponibili
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Optimization of A Simple Aircraft Wing
Editore:
LAP LAMBERT Academic Publishing, 2019
ISBN 10: 6139458048
ISBN 13: 9786139458042
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Brossura
Da: moluna, Greven, Germania
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Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Srinivasa Rao DokkuDokku Srinivasa Rao(Ph.D),M.Tech(CAD/CAM),B.E(Mech),D.M.E,M.I.E(India),ISHRAE(India).Pursuing Ph.D from Andhra University,Completed M.Tech (CAD/CAM) from GITAM,B.E(Mech) from M.V.S.R.Engg.College affiliated to Osma. Codice articolo 385859400
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Optimization of A Simple Aircraft Wing
Editore:
LAP LAMBERT Academic Publishing Mrz 2019, 2019
ISBN 10: 6139458048
ISBN 13: 9786139458042
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Taschenbuch
Da: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germania
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Taschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -In this parametric study the aircraft wing model was designed to a light weight, comfortable model which is also cost effective than the some of the existing models around the world. On testing the wing by applying uniformly distributed load, the Equivalent Stresses and the Total Deformations are calculated.The design of experiments was generated using central composite design method and subsequent optimization is carried out using screening method. Duly considered Aluminium material has the values of weight as 1050kg, 25985384.62 equivalent stresses. Now these values are optimized by 10% to the originally obtained values. The optimized values are, weight of leg is 948.2 kg, equivalent stresses are 2.8163E+07 and deformation is 0.81606m.Optimization problem was investigated in this paper. It is noticed that even though the basic geometry and the same sets of design variables are used, problem has radicaldifference with respect to design sensitivity. Optimized Problem possesses high sensitivity with respect to sizing design variables. Generally, it is not possible to determine beforehand which subset of design variables will be dominant in terms of sensitivity. 72 pp. Englisch. Codice articolo 9786139458042
Quantità: 1 disponibili
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Optimization of A Simple Aircraft Wing
Editore:
LAP LAMBERT Academic Publishing Mär 2019, 2019
ISBN 10: 6139458048
ISBN 13: 9786139458042
Nuovo
Taschenbuch
Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germania
Valutazione del venditore 5 su 5 stelle
Taschenbuch. Condizione: Neu. Neuware -In this parametric study the aircraft wing model was designed to a light weight, comfortable model which is also cost effective than the some of the existing models around the world. On testing the wing by applying uniformly distributed load, the Equivalent Stresses and the Total Deformations are calculated.The design of experiments was generated using central composite design method and subsequent optimization is carried out using screening method. Duly considered Aluminium material has the values of weight as 1050kg, 25985384.62 equivalent stresses. Now these values are optimized by 10% to the originally obtained values. The optimized values are, weight of leg is 948.2 kg, equivalent stresses are 2.8163E+07 and deformation is 0.81606m.Optimization problem was investigated in this paper. It is noticed that even though the basic geometry and the same sets of design variables are used, problem has radicaldifference with respect to design sensitivity. Optimized Problem possesses high sensitivity with respect to sizing design variables. Generally, it is not possible to determine beforehand which subset of design variables will be dominant in terms of sensitivity.Books on Demand GmbH, Überseering 33, 22297 Hamburg 72 pp. Englisch. Codice articolo 9786139458042
Quantità: 2 disponibili
Immagini fornite dal venditore
Optimization of A Simple Aircraft Wing
Editore:
LAP LAMBERT Academic Publishing, 2019
ISBN 10: 6139458048
ISBN 13: 9786139458042
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 - In this parametric study the aircraft wing model was designed to a light weight, comfortable model which is also cost effective than the some of the existing models around the world. On testing the wing by applying uniformly distributed load, the Equivalent Stresses and the Total Deformations are calculated.The design of experiments was generated using central composite design method and subsequent optimization is carried out using screening method. Duly considered Aluminium material has the values of weight as 1050kg, 25985384.62 equivalent stresses. Now these values are optimized by 10% to the originally obtained values. The optimized values are, weight of leg is 948.2 kg, equivalent stresses are 2.8163E+07 and deformation is 0.81606m.Optimization problem was investigated in this paper. It is noticed that even though the basic geometry and the same sets of design variables are used, problem has radicaldifference with respect to design sensitivity. Optimized Problem possesses high sensitivity with respect to sizing design variables. Generally, it is not possible to determine beforehand which subset of design variables will be dominant in terms of sensitivity. Codice articolo 9786139458042
Quantità: 1 disponibili