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Excerpt from The Triplane and the Stable Biplane
The following aerodynamical investigation was under taken to determine the suitability of the triplane arrange ment for weight-carrying as compared with the biplane. It appears that the triplane is not so effective as the biplane, and will require somewhat more power to drive; but with sufficient power the triplane can support nearly the same weight as the biplane at its attitude of maximum lift. The loss is only about per cent. At small angles near 4 deg, for the same lift the trip-lane requires some 6 per cent. More power than the corresponding biplane. At 4 deg. Incidence the ratio of lift to resistance is for the biplane against for the triplane.
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- EditoreForgotten Books
- Data di pubblicazione2018
- ISBN 10 1334123047
- ISBN 13 9781334123047
- RilegaturaCopertina flessibile
- LinguaInglese
- Numero di pagine48
- Contatto del produttorenon disponibile
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The Triplane and the Stable Biplane Classic Reprint
Da: PBShop.store US, Wood Dale, IL, U.S.A.
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PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000. Codice articolo LX-9781334123047
Quantità: 15 disponibili
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The Triplane and the Stable Biplane Classic Reprint
Da: PBShop.store UK, Fairford, GLOS, Regno Unito
Valutazione del venditore 4 su 5 stelle
PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000. Codice articolo LX-9781334123047
Quantità: 15 disponibili
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The Triplane and the Stable Biplane (Classic Reprint)
Print on DemandDa: Forgotten Books, London, Regno Unito
Valutazione del venditore 5 su 5 stelle
Paperback. Condizione: New. Print on Demand. This book explores the aerodynamic properties of a triplane aeroplane in comparison to biplane designs. The outcome from the author's experiments aid understanding of weight-carrying capabilities and wing design for flight stability and efficiency. The author conducted wind tunnel experiments to measure lift and resistance of various wing models, including monoplanes, biplanes and the triplane design. Results of the tests revealed that, at small angles of attack, the triplane design offered lower lift than biplane configurations. However, for greater angles of incidence near 16 degrees, the triplane exhibited a significant advantage in stalling behaviour and reduced resistance. The book also presents valuable data on lift/drift ratios and centre of pressure movement for the different wing configurations, providing insights that are applicable to designing and constructing stable and efficient aircraft. This book is a reproduction of an important historical work, digitally reconstructed using state-of-the-art technology to preserve the original format. In rare cases, an imperfection in the original, such as a blemish or missing page, may be replicated in the book. print-on-demand item. Codice articolo 9781334123047_0
Quantità: Più di 20 disponibili