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Propeller Characteristics and Slipstream Effects on a High Wing Monoplane From Wind Tunnel Tests: Thesis (Classic Reprint) - Softcover

 
9780282856229: Propeller Characteristics and Slipstream Effects on a High Wing Monoplane From Wind Tunnel Tests: Thesis (Classic Reprint)

Synopsis

Excerpt from Propeller Characteristics and Slipstream Effects on a High Wing Monoplane From Wind Tunnel Tests: Thesis

The principal advantages of a powered model test over a full scale flight test are ease of control and facility in measuring the forces and moments develone( In the wind tunnel, power output results are read on the external balance system as in a normal Wind tunnel test. The six component system is shown in Vigure 1, Here, air velocity, geometrical angle of attack, thrust, drag, lift and moments are measured. The measurement of power input is more complicated and is accomplished by means of a revolution co'nter and a torque meter.

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This book is a reproduction of an important historical work. Forgotten Books uses state-of-the-art technology to digitally reconstruct the work, preserving the original format whilst repairing imperfections present in the aged copy. In rare cases, an imperfection in the original, such as a blemish or missing page, may be replicated in our edition. We do, however, repair the vast majority of imperfections successfully; any imperfections that remain are intentionally left to preserve the state of such historical works.

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  • PublisherForgotten Books
  • Publication date2018
  • ISBN 10 0282856226
  • ISBN 13 9780282856229
  • BindingPaperback
  • LanguageEnglish
  • Number of pages77

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9781014650931: Propeller Characteristics and Slipstream Effects on a High Wing Monoplane From Wind Tunnel Tests

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ISBN 10:  1014650933 ISBN 13:  9781014650931
Publisher: Hassell Street Press, 2021
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James Sargent Russell, H. M. McCoy
Published by Forgotten Books, 2018
ISBN 10: 0282856226 ISBN 13: 9780282856229
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Paperback. Condition: New. Print on Demand. This book centers on a crucial and innovative method of testing model aircraft in a wind tunnel. The technique, termed powered model testing, grants researchers exceptional control over measurements of forces influencing an aircraft's flight, opening up new avenues for studying propeller characteristics. It allows for the precise analysis of thrust, drag, lift, and moments, enabling researchers to evaluate the effectiveness of different propeller designs and their impact on aircraft performance. The author meticulously details the apparatus and methodology employed in powered model testing, providing valuable insights into the intricacies of wind tunnel experimentation. This book offers an in-depth exploration of propeller theory and its practical applications, making it an essential resource for engineers, researchers, and anyone interested in aircraft design and development. 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. Seller Inventory # 9780282856229_0

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ISBN 10: 0282856226 ISBN 13: 9780282856229
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James Sargent Russell
Published by Forgotten Books, 2018
ISBN 10: 0282856226 ISBN 13: 9780282856229
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