Reliability considerations in the design, assembly, and testing of the mariner iv power system
Reliability considerations in design, assembly, and testing of Mariner IV power system
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Reliability considerations in design, assembly, and testing of Mariner IV power system
Design considerations of astronomical telescopes for lunar surface observation
Topological considerations and synthesis of linear networks by means of method of structural numbers
Aerospace medical and bioengineering considerations in M-2 lifting body research vehicle, discussing protective equipment, escape and medical monitoring systems
Two-electron spectra with consideration of four pure coupling types in study of energy level structure, relative line strengths and Lande g factors
Energy considerations in stability analysis of discrete linear structural systems under nonconservative forces
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The design of lightweight, efficient structures is one of the fundamental requirements for achievement of high performance in military aircraft. In this paper some of the structural and materials considerations that are important to the strength, weight, and integrity of aircraft structures are reviewed. A comparison of some structural materials is made on the basis of weight-strength and tear resistance. In the area of structural design, the relative weights of several types of construction that are of current interest are reviewed and the influence of different materials and the effects of the related temperatures on structural weight are indicated. Lastly, other factors that are of importance in structural design of future aircraft are discussed. These include strength under nonuniform temperatures, creep, sonic fatigue, and panel flutter.