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Airframe Structural Design: Practical Design Information and by Michael Chun-Yung Niu, Mike Niu PDF

By Michael Chun-Yung Niu, Mike Niu

This e-book represents a number of a long time of knowledge assortment, examine, conversations with diverse airframe experts, plus the author's greater than twenty years' event in airframe structural layout. From structural point of view, the e-book is meant for use as a device to assist in achieving structural integrity in accordance with govt laws, requirements, standards, etc., for designing advertisement or army transports, army opponents, in addition to basic aviation airplane. it may be regarded as a troubleshooting advisor for airline structural upkeep and service engineers or as a supplementary instruction manual in instructing plane structural layout in university. This publication is split right into a overall of 16 bankruptcy and emphasizes itemized write-ups, tables, graphs and illustrations to steer on to sights. the knowledge can be utilized for designing and sizing airframe constructions and, anyplace wanted, instance calculations are offered for rationalization.

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Additional resources for Airframe Structural Design: Practical Design Information and Data on Aircraft Structures (1st edition)

Sample text

The power given by the torques and angular velocities terms are: (33) reorganizing the terms the result is: Hence, the equivalence of mechanical power gives the equality, 40 Y 004102812004 - or in a simplified form, ,=I( 4 - j p=l Trqp are the generalized torque forces. The dependence of the angular velocities av k ae, a n d xit - -aqPp, ' c--kjp,~+p aqp on the components of the angular velocity on the mobile p-1aqp system of reference of body i, ox,,wy1,o,, can be derived by using the equation (2) p-1 p=l aqp A similar procedure as in the case of the angular velocities and torques will be used for the linear forces and velocities.

14, 895-913. C. (1979) Dynamics of chain of flexible bodies, J. Astronaut. , 27(4), 359380. D. (1 98 1) Concepts and Applications of Finite Element Analysis, Second Edition. G. (1995) The Finite Element Method for Engineers, Third Edition, Wiley & Sons. N. (1977) Finite Element Method, The MIT Press. J. (1981) Finite Element Procedures in Engineering Analysis, Prentice Hall. C. (1979) The Finite Element Method, McGraw-Hill. A. D. Thesis, University of Iowa, Iowa City. , (1985) Automated Analysis of Constrained Inertia-Variant Flexible Systems, ASME Journal of Vibration, Acoustics, Stress and Reliability in Design, 107(4), 43 1-440.

For this case the choice is the fixed plane XOZ with the transformation having the nodal axis identical to the fixed X axis. Thus, the mobile system is rotated with 90 degrees so that the mobile Z is perpendicular to the fixed XOZ plane. The angle p, defines the position between the fixed X axis (nodal axis) and the mobile Xi axes. Such an example is p5 in Figure 3. The Euler angles yl = 0 , 6,= a12 and the Y direction coordinates remain constant. Hence, the values of the respective velocities and energy are zero.

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Airframe Structural Design: Practical Design Information and Data on Aircraft Structures (1st edition) by Michael Chun-Yung Niu, Mike Niu


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