A Theoretical Analysis of the Effects of Fuel Motion on Airplane Dynamics

A Theoretical Analysis of the Effects of Fuel Motion on Airplane Dynamics

Author: Albert A. Schy

Publisher:

Published: 1951

Total Pages: 62

ISBN-13:

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The general equations of motion for an airplane with a number of spherical fuel tanks are derived. These equations are applied to two cases with two fuel tanks located in the plane of symmetry. The calculated motions show that the airplane motion may be greatly changed by considering the motion of the fuel and, in particular, the small-amplitude residual oscillations may result. The same type of analysis may be applied to arbitrarily shaped tanks; therefore, the most general conclusions as to the effects of the fuel motion on airplane dynamics also apply for arbitrarily shaped tanks.


Report

Report

Author: United States. National Advisory Committee for Aeronautics

Publisher:

Published: 1952

Total Pages: 32

ISBN-13:

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Aircraft Dynamics and Automatic Control

Aircraft Dynamics and Automatic Control

Author: Duane T. McRuer

Publisher: Princeton University Press

Published: 2014-07-14

Total Pages: 809

ISBN-13: 1400855985

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Aeronautical engineers concerned with the analysis of aircraft dynamics and the synthesis of aircraft flight control systems will find an indispensable tool in this analytical treatment of the subject. Approaching these two fields with the conviction that an understanding of either one can illuminate the other, the authors have summarized selected, interconnected techniques that facilitate a high level of insight into the essence of complex systems problems. These techniques are suitable for establishing nominal system designs, for forecasting off-nominal problems, and for diagnosing the root causes of problems that almost inevitably occur in the design process. A complete and self-contained work, the text discusses the early history of aircraft dynamics and control, mathematical models of linear system elements, feedback system analysis, vehicle equations of motion, longitudinal and lateral dynamics, and elementary longitudinal and lateral feedback control. The discussion concludes with such topics as the system design process, inputs and system performance assessment, and multi-loop flight control systems. Originally published in 1974. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.


Technical Note

Technical Note

Author: United States. National Advisory Committee for Aeronautics

Publisher:

Published: 1951

Total Pages: 818

ISBN-13:

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