Da: GreatBookPrices, Columbia, MD, U.S.A.
EUR 15,40
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Aggiungi al carrelloCondizione: New.
Da: BargainBookStores, Grand Rapids, MI, U.S.A.
Paperback or Softback. Condizione: New. Three Component Velocity Measurements in the Tip Vortex of a Micro-Air-Vehicle. Book.
Da: GreatBookPrices, Columbia, MD, U.S.A.
EUR 15,54
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Aggiungi al carrelloCondizione: As New. Unread book in perfect condition.
Da: Ria Christie Collections, Uxbridge, Regno Unito
EUR 16,65
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Aggiungi al carrelloCondizione: New. In.
Da: GreatBookPricesUK, Woodford Green, Regno Unito
EUR 16,64
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Aggiungi al carrelloCondizione: New.
Da: GreatBookPricesUK, Woodford Green, Regno Unito
EUR 19,13
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Aggiungi al carrelloCondizione: As New. Unread book in perfect condition.
Da: moluna, Greven, Germania
EUR 23,23
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Aggiungi al carrelloCondizione: New. KlappentextrnrnAn investigation into the characteristics of the wing tip vortex on a flexible wing micro-air-vehicle (MAV) was conducted. The Air Force Research Lab, Munitions Directorate designed a man-portable MAV with a 24 wingspan and 6 ro.
Da: PBShop.store US, Wood Dale, IL, U.S.A.
EUR 19,22
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.
Lingua: Inglese
Editore: Creative Media Partners, LLC Okt 2012, 2012
ISBN 10: 1249586445 ISBN 13: 9781249586449
Da: AHA-BUCH GmbH, Einbeck, Germania
EUR 27,41
Quantità: 2 disponibili
Aggiungi al carrelloTaschenbuch. Condizione: Neu. Neuware - An investigation into the characteristics of the wing tip vortex on a flexible wing micro-air-vehicle (MAV) was conducted. The Air Force Research Lab, Munitions Directorate designed a man-portable MAV with a 24' wingspan and 6' root chord to be used for battle damage assessment and reconnaissance or local surveillance. For this MAV, two prototypes have been produced. One has a rigid wing prepared from carbonfiber; the other has a flexible wing prepared from parachute-latex material attached to a carbon-fiber frame. The experiments were performed to investigate the wing displacement and wing tip vortex interaction, characterizing the differences and effects of wing displacement and the shifting and velocity of wing tip vortex between two prototypes placed in typical operating conditions. Initially, each aircraft model was mounted at the test section in the low speed wind tunnel and exposed to various angles of attack and wind conditions. An optical telescope was used to measure the wing tip displacement and a tri-axial hot-wire anemometer was used to capture the velocity profiles in the wind tunnel to characterize wing tip vortex system. The results indicate that the wing tip displacement of the flexible wing was approximately 8 times than that of the rigid wing in an unstalled condition. The data suggests that flexible wing has a denser core-distribution of velocity within the wing tip vortex and delays the angle at which separation occurs.
Da: PBShop.store UK, Fairford, GLOS, Regno Unito
EUR 18,23
Quantità: Più di 20 disponibili
Aggiungi al carrelloPAP. Condizione: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
Da: Majestic Books, Hounslow, Regno Unito
EUR 22,82
Quantità: 4 disponibili
Aggiungi al carrelloCondizione: New. Print on Demand pp. 92.
Da: Books Puddle, New York, NY, U.S.A.
Condizione: New. Print on Demand pp. 92.
Da: Biblios, Frankfurt am main, HESSE, Germania
EUR 23,36
Quantità: 4 disponibili
Aggiungi al carrelloCondizione: New. PRINT ON DEMAND pp. 92.
Da: THE SAINT BOOKSTORE, Southport, Regno Unito
EUR 51,04
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Aggiungi al carrelloPaperback / softback. Condizione: New. This item is printed on demand. New copy - Usually dispatched within 5-9 working days.