Add to ORKGThe development of graphite-epoxy composite structures for use on commercial transport aircraft is considered. Six components, three secondary structures, and three primary structures, are presently under development. The six components are described along with some of the key features of the composite designs and their projected weight savings
The long-term durability of those advanced composite materials which are applicable to aircraft stru...
The Boeing 777 is the first of a new family of wide body airplanes. The new large twin is sized to a...
Composite materials may reduce the final weight of the aircraft structural components, in addition t...
The Advanced Composites Technology (ACT) program is seeking research breakthroughs that will allow s...
A multifaceted program is described in which aeronautical, mechanical, and materials engineers inter...
The use of filamentary composite materials in the design and construction of primary aircraft struct...
Preliminary weight and cost estimates have been prepared for design concepts utilized for a transoni...
Structural weight savings using advanced composites have been demonstrated for many years. Most mili...
This paper provides a brief overview of the NASA Advanced Composites Technology (ACT) Program. Criti...
The NASA Aircraft Energy Efficiency (ACEE) Composite Primary Aircraft Structures Program has made si...
The development and flight evaluation of an advanced composite empennage component is presented. The...
Results of tests conducted to demonstrate that composite structures save weight, possess long term d...
Commercial aircraft manufacturers are making production commitments to composite structure for futur...
Toppics addressed include: advanced composites on Boeing commercial aircraft; composite wing durabil...
In this paper, the aircraft and space vehicle requirements for composite structures are compared. It...
The long-term durability of those advanced composite materials which are applicable to aircraft stru...
The Boeing 777 is the first of a new family of wide body airplanes. The new large twin is sized to a...
Composite materials may reduce the final weight of the aircraft structural components, in addition t...
The Advanced Composites Technology (ACT) program is seeking research breakthroughs that will allow s...
A multifaceted program is described in which aeronautical, mechanical, and materials engineers inter...
The use of filamentary composite materials in the design and construction of primary aircraft struct...
Preliminary weight and cost estimates have been prepared for design concepts utilized for a transoni...
Structural weight savings using advanced composites have been demonstrated for many years. Most mili...
This paper provides a brief overview of the NASA Advanced Composites Technology (ACT) Program. Criti...
The NASA Aircraft Energy Efficiency (ACEE) Composite Primary Aircraft Structures Program has made si...
The development and flight evaluation of an advanced composite empennage component is presented. The...
Results of tests conducted to demonstrate that composite structures save weight, possess long term d...
Commercial aircraft manufacturers are making production commitments to composite structure for futur...
Toppics addressed include: advanced composites on Boeing commercial aircraft; composite wing durabil...
In this paper, the aircraft and space vehicle requirements for composite structures are compared. It...
The long-term durability of those advanced composite materials which are applicable to aircraft stru...
The Boeing 777 is the first of a new family of wide body airplanes. The new large twin is sized to a...
Composite materials may reduce the final weight of the aircraft structural components, in addition t...