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Aircraft wing

Products can be found in every principal market area including rocket motor and shell casings, air and gas pressure tanks, aircraft wing fuel tanks, utihty poles, automotive and tmck drive shafts, sailboat masts, vaulting poles, fishing rods, golf shafts, railroad tanks cars, and pipes and tanks for oil, gas, and chemical processing. [Pg.97]

A batch of 7000 series aluminium alloy rivets for an aircraft wing was inadvertently over-aged. What steps can be taken to reclaim this batch of rivets ... [Pg.112]

There are no hard-and-fast rules to follow in setting safety factors for any given material unless experience exists. The most important consideration is of course the probable consequences of failure. For example, a little extra deflection in an outside wall or a hairline crack in one of six internal screw bosses might not cause concern, but the failure of a pressure vessel or aircraft wing might have serious safety or product-liability implications. [Pg.130]

When a fluid flows past a solid surface, the velocity of the fluid in contact with the wall is zero, as must be the case if the fluid is to be treated as a continuum. If the velocity at the solid boundary were not zero, the velocity gradient there would be infinite and by Newton s law of viscosity, equation 1.44, the shear stress would have to be infinite. If a turbulent stream of fluid flows past an isolated surface, such as an aircraft wing in a large wind tunnel, the velocity of the fluid is zero at the surface but rises with increasing distance from the surface and eventually approaches the velocity of the bulk of the stream. It is found that almost all the change in velocity occurs in a very thin layer of fluid adjacent to the solid surface ... [Pg.64]

Aircraft Wing-Tip Flares — intended for signalling and assisting planes in landing. [Pg.445]

Atmospheric effects of large-scale TNT expins have also been studied in depth both practically and theoretically. Factors considered include pressure and impulse effects, decay characteristics and travel and duration times, all as a function of distance, and for both free-field and reflection situations (Refs 3,9,15,16, 17,24,32, 33,34,35,36,44, 53,75,76,115 116). A distinction is made between the blast area dose to the source, comprising air and the products of expln, and that farther away involving air only (Ref 53). Double-burst conditions (fireball and shock wave interaction, and torus formation) have been studied (Ref 149), as have also the dynamics of dust formation and motion (Refs 25,26 117). Performance tests were run on a naval blast valve (Ref 92), and on aircraft wing panels (Ref 4)... [Pg.765]

Stiff lightweight structures such as aircraft wings are made from sandwiches of continuous sheets filled with foams or honeycombs. Open porous structures can form frameworks for infiltration by other materials leading to application of biocompatible implants. Open pore structures are used as supports for catalysts. [Pg.202]

New aluminum alloys containing 3% lithium with small amounts of zinc and magnesium may supplant 2024 and 7075 in the aircraft wings and fuselage. [Pg.235]

Esters are widely used in industry as solvents. Ethyl acetate is a good solvent for a wide variety of compounds, and its toxicity is low compared with other solvents. Ethyl acetate is also found in household products such as cleaners, polishes, glues, and spray finishes. Ethyl butyrate and butyl butyrate were once widely used as solvents for paints and finishes, including the butyrate dope that was sprayed on the fabric covering of aircraft wings to make them tight and stiff. Polyesters (covered later in this section and in Chapter 26) are among the most common polymers, used in fabrics (Dacron ), films (VCR tapes), and solid plastics (soft-drink bottles). [Pg.1024]

Product X947-400QSV231 Aircraft Wing Assembly Date 10/08/08 ... [Pg.266]

These could be found, for example, in zed section stringers or parts of rib-elements in aircraft wings. In-situ testing of small, approximately 2mm wide sections, of such structures was performed on an optical microscope using a Minimat miniature materials tester [18]... [Pg.283]

Fig. 4. Phosphorescent image of a section of a model aircraft wing showing the surface pressure distribution as a function of tilt angle (a) during a wind tunnel experiment. (The colors, whilst artificial, reflect the pressure at different points on the surface. In this case, the polymer matrix was composed of poly(aminothionylphosphazene)-b-poly[THF] (31) and the dye was [Ru(phenPh2)3]Cl2. The images were obtained from a series of tests run at the National Research Council Wind Tunnel in Ottawa)... Fig. 4. Phosphorescent image of a section of a model aircraft wing showing the surface pressure distribution as a function of tilt angle (a) during a wind tunnel experiment. (The colors, whilst artificial, reflect the pressure at different points on the surface. In this case, the polymer matrix was composed of poly(aminothionylphosphazene)-b-poly[THF] (31) and the dye was [Ru(phenPh2)3]Cl2. The images were obtained from a series of tests run at the National Research Council Wind Tunnel in Ottawa)...
Cellulose acetate Doping for aircraft wings, safety film, synthetic textiles Rayon, Celanese, Tricel... [Pg.186]

Aircraft Wing Tank Sealant - Low temperature flexibility, solvent resistance, adhesion to aluminum and other aircraft metal surfaces. [Pg.153]


See other pages where Aircraft wing is mentioned: [Pg.713]    [Pg.401]    [Pg.95]    [Pg.11]    [Pg.29]    [Pg.70]    [Pg.379]    [Pg.379]    [Pg.421]    [Pg.110]    [Pg.127]    [Pg.82]    [Pg.87]    [Pg.286]    [Pg.436]    [Pg.336]    [Pg.109]    [Pg.95]    [Pg.455]    [Pg.286]    [Pg.606]    [Pg.455]    [Pg.21]    [Pg.22]    [Pg.23]    [Pg.138]    [Pg.564]    [Pg.455]    [Pg.775]    [Pg.726]    [Pg.441]    [Pg.797]   
See also in sourсe #XX -- [ Pg.18 ]




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