Da: GreatBookPrices, Columbia, MD, U.S.A.
EUR 15,54
Quantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New.
Da: GreatBookPrices, Columbia, MD, U.S.A.
EUR 15,55
Quantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: As New. Unread book in perfect condition.
Da: BargainBookStores, Grand Rapids, MI, U.S.A.
Paperback or Softback. Condizione: New. Validation of Design and Analysis Techniques of Tailored Composite Structures. Book.
Da: Ria Christie Collections, Uxbridge, Regno Unito
EUR 16,82
Quantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New. In.
Da: GreatBookPricesUK, Woodford Green, Regno Unito
EUR 16,80
Quantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New.
Da: GreatBookPricesUK, Woodford Green, Regno Unito
EUR 19,33
Quantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: As New. Unread book in perfect condition.
Condizione: Very Good. Item in very good condition! Textbooks may not include supplemental items i.e. CDs, access codes etc.
Da: GreatBookPrices, Columbia, MD, U.S.A.
EUR 44,50
Quantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New.
Da: GreatBookPrices, Columbia, MD, U.S.A.
EUR 45,51
Quantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: As New. Unread book in perfect condition.
Condizione: New. Introduction to the Design and Analysis of Composite Structures: An Engineers Practical Guide Using OptiStruct (Paperback or Softback).
Lingua: Inglese
Editore: LAP Lambert Academic Publishing, 2010
ISBN 10: 3838351843 ISBN 13: 9783838351841
Da: GreatBookPrices, Columbia, MD, U.S.A.
EUR 48,83
Quantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New.
Lingua: Inglese
Editore: LAP Lambert Academic Publishing, 2010
ISBN 10: 3838351843 ISBN 13: 9783838351841
Da: GreatBookPrices, Columbia, MD, U.S.A.
EUR 50,66
Quantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: As New. Unread book in perfect condition.
Lingua: Inglese
Editore: LAP Lambert Academic Publishing, 2010
ISBN 10: 3838351843 ISBN 13: 9783838351841
Da: Ria Christie Collections, Uxbridge, Regno Unito
EUR 47,76
Quantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New. In.
Lingua: Inglese
Editore: LAP Lambert Academic Publishing 2010-03-29, 2010
ISBN 10: 3838351843 ISBN 13: 9783838351841
Da: Chiron Media, Wallingford, Regno Unito
EUR 45,06
Quantità: 10 disponibili
Aggiungi al carrelloPaperback. Condizione: New.
Prima edizione
EUR 28,87
Quantità: 1 disponibili
Aggiungi al carrelloHard Cover. Condizione: Good. No Jacket. First Edition. From an academic library with the usual stamps etc.
Condizione: good.
Lingua: Inglese
Editore: LAP Lambert Academic Publishing, 2010
ISBN 10: 3838351843 ISBN 13: 9783838351841
Da: GreatBookPricesUK, Woodford Green, Regno Unito
EUR 47,75
Quantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New.
Da: GreatBookPricesUK, Woodford Green, Regno Unito
EUR 52,34
Quantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: As New. Unread book in perfect condition.
Lingua: Inglese
Editore: LAP Lambert Academic Publishing, 2010
ISBN 10: 3838351843 ISBN 13: 9783838351841
Da: GreatBookPricesUK, Woodford Green, Regno Unito
EUR 54,11
Quantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: As New. Unread book in perfect condition.
Lingua: Inglese
Editore: Amer Inst of Aeronautics &, 2010
ISBN 10: 1600867804 ISBN 13: 9781600867804
Da: GoldBooks, Denver, CO, U.S.A.
Hardcover. Condizione: new. New Copy. Customer Service Guaranteed.
Da: GreatBookPricesUK, Woodford Green, Regno Unito
EUR 57,08
Quantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: New.
Da: moluna, Greven, Germania
EUR 23,29
Quantità: Più di 20 disponibili
Aggiungi al carrelloKartoniert / Broschiert. Condizione: New. KlappentextrnrnAeroelasticity is the relationship between the elasticity of an aircraft structure and its aerodynamics. This relationship can cause instabilities such as flutter in a wing. Engineers have long studied aeroelasticity to ensure suc.
Da: Zubal-Books, Since 1961, Cleveland, OH, U.S.A.
Condizione: Good. 634 pp., hardcover, ex library, else text clean and binding tight. - If you are reading this, this item is actually (physically) in our stock and ready for shipment once ordered. We are not bookjackers. Buyer is responsible for any additional duties, taxes, or fees required by recipient's country.
Condizione: Brand New. New. US edition. Expediting shipping for all USA and Europe orders excluding PO Box. Excellent Customer Service.
Da: Books Puddle, New York, NY, U.S.A.
Condizione: New. pp. 448.
Lingua: Inglese
Editore: British Library, Historical Print Editions, 2013
ISBN 10: 1288910614 ISBN 13: 9781288910618
Da: PBShop.store US, Wood Dale, IL, U.S.A.
EUR 19,36
Quantità: Più di 20 disponibili
Aggiungi al carrelloPAP. Condizione: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
ISBN 10: 1041322321 ISBN 13: 9781041322320
Da: Basi6 International, Irving, TX, U.S.A.
Condizione: Brand New. New.SoftCover International edition. Different ISBN and Cover image but contents are same as US edition.Expediting shipping for all USA and Europe orders excluding PO Box. Excellent Customer Service.
Da: Majestic Books, Hounslow, Regno Unito
EUR 79,76
Quantità: 4 disponibili
Aggiungi al carrelloCondizione: New. pp. 448.
Da: Romtrade Corp., STERLING HEIGHTS, MI, U.S.A.
Condizione: New. This is a Brand-new US Edition. This Item may be shipped from US or any other country as we have multiple locations worldwide.
Lingua: Inglese
Editore: British Library, Historical Print Editions Mär 2013, 2013
ISBN 10: 1288910614 ISBN 13: 9781288910618
Da: AHA-BUCH GmbH, Einbeck, Germania
EUR 27,41
Quantità: 2 disponibili
Aggiungi al carrelloTaschenbuch. Condizione: Neu. Neuware - Aeroelasticity is the relationship between the elasticity of an aircraft structure and its aerodynamics. This relationship can cause instabilities such as flutter in a wing. Engineers have long studied aeroelasticity to ensure such instabilities do not become a problem within normal operating conditions. In recent decades structural tailoring has been used to take advantage of aeroelasticity. It is possible to tailor an aircraft structure to respond favorably to multiple different flight regimes such as takeoff, landing, cruise, 2-g pull up, etc. Structures can be designed so that these responses provide an aerodynamic advantage. This research investigates the ability to design and analyze tailored structures made from filamentary composites. Specifically the accuracy of tailored composite analysis must be verified if this design technique is to become feasible. To pursue this idea, a validation experiment has been performed on a small-scale filamentary composite wing box. The box is tailored such that its cover panels induce a global bend-twist coupling under an applied load. Two types of analysis were chosen for the experiment. The first is a closed form analysis based on a theoretical model of a single cell tailored box beam and the second is a finite element analysis. The predicted results are compared with the measured data to validate the analyses. The comparison of results show that the finite element analysis is capable of predicting displacements and strains to within 10% on the small-scale structure. The closed form code is consistently able to predict the wing box bending to 25% of the measured value. This error is expected due to simplifying assumptions in the closed form analysis. Differences between the closed form code representation and the wing box specimen caused large errors in the twist prediction. The closed form analysis prediction of twist has not been validated from this test.