Transcription of Chapter 8 Weight Estimation - Virginia Tech
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72 Chapter 8 Weight IntroductionStatistical Weight equations, although capable of producing landing gear group weightsquickly and generally accurately, do not respond to all the variations in landing gear designparameters. In addition, the equations are largely dependent on the database of existingaircraft. For future large aircraft, such Weight data is virtually non-existent. Thus, it isdesirable that an analytical Weight Estimation method which is more sensitive thanstatistical methods to variations in the design of the landing gear should be adopted. Theobjectives are to allow for parametric studies involving key design considerations that drivelanding gear Weight , and to establish crucial Weight gradients to be used in the on the procedures described in this Chapter , algorithms were developed to sizeand estimate the Weight of the structural members of the landing gear .
Chapter 8 Weight Estimation 8.1. Introduction ... landing gear weight, and to establish crucial weight gradients to be used in the optimization ... The locations of structural components are established by means of known length and/or point locations, and each point-to-point
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11: Landing Gear & Components, Landing gear, CHAPTER 32 - Landing Gear, CHAPTER 32 LANDING GEAR, Components, Chassis Parts Manual, LANDING GEAR COMPONENTS, Landing Gear Landing Gear Landing Gear, CRJ 700/900 Landing Gear, DELTA, CHAPTER 13 LANDING GEAR, Landing Systems, Chapter 3 Landing Gear Concept Selection, DTIC