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Author: S. L. Walkden
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 280
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Book Description
Author: S. L. Walkden
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 280
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Book Description
Author: S.L. Walkden
Publisher:
ISBN:
Category :
Languages : en
Pages : 388
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Book Description
Author: H. Hoene
Publisher:
ISBN:
Category : Equations of motion
Languages : en
Pages : 740
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Book Description
The equations of motion for an airplane penetrating a gust are derived using a few simplifying assumptions. Calculations of loads for different static longitudinal stability on two German airplane models, HC 45 and HS 122, are compared with flight tests. Good agreement is obtained between the trend of the flight tests and the calculated values; however no absolute comparison was possible between the flight tests and calculations.
Author: Frederic M. Hoblit
Publisher: AIAA
ISBN: 9781600860607
Category : Airplanes
Languages : en
Pages : 332
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Book Description
Author: Robert T. Jones
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
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Book Description
Author: S. L. Walkden
Publisher:
ISBN: 9781331993759
Category : Technology & Engineering
Languages : en
Pages : 282
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Book Description
Excerpt from Aeroplanes in Gusts: Soaring Flight and the Stability of Aeroplanes The Path op the Wind; Mechanical Analogies to Soaring; Velocity Soaring; Stationary Soaring, General Velocity Soaring; The Policy op the Soaring Bird; Comparison of Soaring and Non-Soaring Birds; Human Soaring; Automatic Stability and Soaring, Practical Lines of Development, Automatic Wheeling Soaring; Reprinted Articles; I. Propellers as Stabilisers, II. Propellers as Disturbers of Stability, III. Longitudinal Stability in Gusts; "Fly Ability" and "Stability"; The Nature or Gravity; The Analogy between Ship Stability and Aeroplane Stability; The Self-Righting Property in Still Air; An Informal Practical Explanation, A Formal Graphical Explanation, Explanations to receive with Caution, Oscillations, Formula relating to Circling; Appendix; Aviation Disasters; Disasters caused by Front-heaviness; Disasters caused by an Inverse Stable Attitude; Disasters caused by the Pilot's Weight on his Controls; Combinations of Causes; Unpractical Lines of Development About the Publisher Forgotten Books publishes hundreds of thousands of rare and classic books. Find more at www.forgottenbooks.com 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.
Author: John C. Houbolt
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 94
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Book Description
Through the use of difference equations and matrix notation a systematic procedure is developed for the calculation of the structural response of an aircraft flying through a gust. The method takes into account wing bending and twisting flexibilities, fuselage flexibility, vertical and pitching motion of the airplane, and some tail forces. Strip theory is used, but approximate three-dimensional and compressibility corrections can be made without difficulty. Either sharp-edge or arbitrary gusts may be treated.
Author: C. Thomas Snyder
Publisher:
ISBN:
Category : Aeronautics in meteorology
Languages : en
Pages : 26
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Book Description
Author: Waunnetta Keene Walling
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 92
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Book Description
Author: S L Walkden
Publisher: Palala Press
ISBN: 9781359049018
Category :
Languages : en
Pages :
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Book Description
This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it. This work was reproduced from the original artifact, and remains as true to the original work as possible. Therefore, you will see the original copyright references, library stamps (as most of these works have been housed in our most important libraries around the world), and other notations in the work.This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.As a reproduction of a historical artifact, this work may contain missing or blurred pages, poor pictures, errant marks, etc. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
