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aircraft structures

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Journal Articles
Alloy Digest (1986) 35 (7): Al-269.
Published: 01 July 1986
... UNS No. A97075 is a wrought precipitation-hardenable aluminum alloy. It has excellent mechanical properties, workability and response to heat treatment and refrigeration. Its typical uses comprise aircraft structural parts and other highly stressed structural applications where very high strength...
Journal Articles
Alloy Digest (1999) 48 (1): Al-357.
Published: 01 January 1999
... Kaiser Aluminum Alloy 2024 has good machinability and good mechanical properties. The alloy is typically used in aircraft structures, rivets, connectors, hydraulic valve bodies, and miscellaneous structural applications. This datasheet provides information on composition, physical properties...
Journal Articles
Alloy Digest (1999) 48 (12): Al-365.
Published: 01 December 1999
... Kaiser Aluminum Alloy 7049 has high mechanical properties and good machinability. The alloy offers a resistance to stress-corrosion cracking and is typically used in aircraft structural parts. This datasheet provides information on composition, physical properties, hardness, tensile properties...
Journal Articles
Alloy Digest (2000) 49 (1): Al-366.
Published: 01 January 2000
... Kaiser Aluminum Alloy 7050 has very high mechanical properties including tensile strength, high fracture toughness, and a high resistance to exfoliation and stress-corrosion cracking. The alloy is typically used in aircraft structural parts. This datasheet provides information on composition...
Journal Articles
Alloy Digest (2002) 51 (11): Al-382.
Published: 01 November 2002
... Alcotec weld filler wire 2319 is a heat treatable wire. The principal alloying elements are copper, manganese, vanadium, zirconium, and titanium. Weld filler wire 2319 was developed primarily for aircraft structural components to weld the high-strength age-hardenable wrought alloy 2219...
Journal Articles
Alloy Digest (1968) 17 (4): SA-225.
Published: 01 April 1968
... for applications such as rocket motor cases and accessories, bolts and fasteners and aircraft structural components- particularly landing gear. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes...
Journal Articles
Alloy Digest (2006) 55 (11): Al-402.
Published: 01 November 2006
... Aluminum alloy 7449 in the T7651 temper is solution heat treated, stress relieved, and overaged. This processing produces an alloy of high strength, good corrosion/exfoliation resistance, and good toughness. An application of interest is the upper-wing skin of aircraft structures. This datasheet...
Journal Articles
Alloy Digest (2016) 65 (7): Al-443.
Published: 01 July 2016
... Kaiser Alloy 7X49 is used in aircraft structural parts. The alloy has characteristics of high strength and good machinability. Good resistance to stress-corrosion cracking in –T7 type temper. X represents either or 1 or 0 as noted in the tex This datasheet provides information on composition...
Journal Articles
Alloy Digest (1963) 12 (6): Ti-35.
Published: 01 June 1963
... Republic RS-110A is a titanium alloy containing manganese as its principle alloying element. The alloy is a medium strength, highly formable sheet alloy which has been used extensively as an aircraft structural material. This datasheet provides information on composition, physical properties...
Journal Articles
Alloy Digest (1964) 13 (2): SS-152.
Published: 01 February 1964
... Pyromet X-12 is a martensitic stainless steel offering high strength at both room temperature and high heat. It is recommended for use in jet engines, steam turbines and aircraft structural parts. This datasheet provides information on composition, physical properties, hardness, elasticity...
Journal Articles
Alloy Digest (1984) 33 (2): SS-440.
Published: 01 February 1984
... include aircraft structural members and equipment for the process industries. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining...
Journal Articles
Alloy Digest (1985) 34 (1): SS-457.
Published: 01 January 1985
... (nearly equal to AISI Type 304 stainless steel) and its high degree of resistance to stress-corrosion cracking, it is used in a variety of environments. Typical uses are aircraft structural components, shafts, valve parts and fittings. This datasheet provides information on composition, physical...
Journal Articles
Alloy Digest (2000) 49 (2): Al-367.
Published: 01 February 2000
... Kaiser Aluminum alloy 7149 has very high mechanical properties and good machinability. The alloy offers a high resistance to stress-corrosion cracking (SCC) and is typically used in aircraft structural parts. This datasheet provides information on composition, physical properties, hardness...
Journal Articles
Alloy Digest (2000) 49 (3): Al-368.
Published: 01 March 2000
... Kaiser Aluminum Alloy 7075 has high mechanical properties and, in the T73 and T74 tempers, offers improved corrosion-cracking resistance. The alloy has good machinability. It is typically used in aircraft structural parts. (See also Alloy Digest Al-457, January 2019.) This datasheet provides...
Journal Articles
Alloy Digest (1987) 36 (2): SA-423.
Published: 01 February 1987
... strength levels and excellent notch ductility. Its many uses include aircraft structural assemblies, pressure vessels, shafting, bolts and fasteners, and rocket motor cases. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well...
Journal Articles
Alloy Digest (2016) 65 (10): Al-447.
Published: 01 October 2016
... Kaiser Alloy 7099-T7651 is used in aircraft wing structures as well as fuselage frames. The alloy has characteristics of high strength and high toughness and good resistance to stress-corrosion cracking. This datasheet provides information on composition, physical properties, elasticity, tensile...
Journal Articles
Alloy Digest (1970) 19 (2): SS-234.
Published: 01 February 1970
... ALLEGHENY ALMAR-362 is an age-hardenable martensitic stainless steel recommended for applications requiring high strength and good corrosion resistance, such as aircraft and missile structures, hydraulic and pneumatic equipment components, and in the chemical processing industry. This datasheet...
Journal Articles
Alloy Digest (1981) 30 (4): Ti-82.
Published: 01 April 1981
... at temperatures up to 700 F. Its uses include aircraft sheet components and structural parts. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and bend strength. It also includes information on high temperature performance and corrosion resistance...
Journal Articles
Alloy Digest (1993) 42 (2): SA-321.
Published: 01 February 1993
... optimum cleanliness and preferred ingot structure. Its applications include aircraft components, pressure vessels and fasteners. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes information...
Journal Articles
Alloy Digest (1962) 11 (5): SA-129.
Published: 01 May 1962
... process without pre-hearing. This process is limited to a maximum thickness of approximately 1 8 . General Characteri sties: Crucible I)6 maintains a very high yield/ultimate srrength ratio up to and including 280,000 psi tensile strength combined with adequate ducriliry for general aircraft structural...