Download 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 numerous a long time of knowledge assortment, learn, conversations with assorted airframe experts, plus the author's greater than twenty years' event in airframe structural layout. From structural perspective, the e-book is meant for use as a device to aid in attaining structural integrity in line with govt laws, necessities, standards, etc., for designing advertisement or army transports, army opponents, in addition to normal aviation airplane. it may be regarded as a troubleshooting advisor for airline structural upkeep and service engineers or as a supplementary instruction manual in educating airplane structural layout in collage. This publication is split right into a overall of 16 bankruptcy and emphasizes itemized write-ups, tables, graphs and illustrations to guide on to sights. the knowledge can be utilized for designing and sizing airframe buildings and, at any place wanted, instance calculations are awarded for rationalization.

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

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Similarly, if the required output signal-to-clutter ratio is (S/C)„, the connection between SCV and MTI improvement factor is PRINCIPLES OF RADAR 35 (S/C)„ cjp or scv I=SCVx(S/C)0 (SIQ0 LR = SCV,, One MTI method uses delay line cancelers, a two-pulse example of which is shown in Fig. 23. Although operation of this clutter canceler can be described with the aid of the Doppler principle, its operation is usually described in the following manner. Radar returns from clutter and a target, produced by the first transmitted radar pulse, load the delay line.

R„ = 304 km. 25 30 RADAR ELECTRONIC WARFARE or remains essentially unchanged, demonstrating the low loss experienced by a 600 MHz signal when propagating through rainfall. It is useful to assume a higher attenuation parameter in order to demon­ strate the method of solution. To this end, it is assumed that a = 5 x 10" 5 . 04 and 7?! 3 - 2 . 5 4 , R2 = 262 km, R3 = 261 km. Many more iterations are required when the rain attenuation is a greater percentage of the total loss. Then, a computer becomes very useful.

Unlike the fan-beam pattern of the TWS radar, the radiation pattern of the coni­ cal-scan (CONSCAN) radar antenna usually has equal beam widths for az­ imuth and elevation. This pattern implies an antenna aperture of roughly equal vertical and horizontal dimensions. As shown in Fig. 32, the an­ tenna pattern, sometimes called a pencil beam, is scanned about a scan axis that intercepts the main beam. Even though this is a conical-scan radar, only an A-scope has been added to the TWS diagram. A range/height dis­ play is now used to acquire the target through a limited-volume search.

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