Add to ORKGThe materials and advanced producibility methods that offer potential structural mass savings in the design of the primary structure for a supersonic cruise aircraft are identified and reported. A summary of the materials and fabrication techniques selected for this analytical effort is presented. Both metallic and composite material systems were selected for application to a near-term start-of-design technology aircraft. Selective reinforcement of the basic metallic structure was considered as the appropriate level of composite application for the near-term design
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 Boeing program entitled Advanced Technology Composite Aircraft Structure (ATCAS) is focused on t...
The analyses performed to provide structural mass estimates for the arrow wing supersonic cruise air...
The structural approach best suited for the design of a Mach 2.7 arrow-wing supersonic cruise aircra...
The design of an economically viable supersonic cruise aircraft requires the lowest attainable struc...
An analytical study was performed to determine the best structural approach for design of primary wi...
The major efforts leading to an efficient structural design include: (1) the analysis methods used t...
A structural design study was conducted to assess the relative merits of structural concepts using a...
Research and development programs provide confidence that technology is in-hand to design an economi...
Preliminary weight and cost estimates have been prepared for design concepts utilized for a transoni...
Studies were conducted to evaluate the cost and weight potential of advanced composite design concep...
The results of four years research on technology are synthesized in an advanced supersonic cruise ai...
Supersonic aircraft designers must shape the outer mold line of the aircraft to improve multiple obj...
Trajectory, load, aerodynamic heating, materials, structural, and thermal analyses for hypersonic cr...
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 Boeing program entitled Advanced Technology Composite Aircraft Structure (ATCAS) is focused on t...
The analyses performed to provide structural mass estimates for the arrow wing supersonic cruise air...
The structural approach best suited for the design of a Mach 2.7 arrow-wing supersonic cruise aircra...
The design of an economically viable supersonic cruise aircraft requires the lowest attainable struc...
An analytical study was performed to determine the best structural approach for design of primary wi...
The major efforts leading to an efficient structural design include: (1) the analysis methods used t...
A structural design study was conducted to assess the relative merits of structural concepts using a...
Research and development programs provide confidence that technology is in-hand to design an economi...
Preliminary weight and cost estimates have been prepared for design concepts utilized for a transoni...
Studies were conducted to evaluate the cost and weight potential of advanced composite design concep...
The results of four years research on technology are synthesized in an advanced supersonic cruise ai...
Supersonic aircraft designers must shape the outer mold line of the aircraft to improve multiple obj...
Trajectory, load, aerodynamic heating, materials, structural, and thermal analyses for hypersonic cr...
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 Boeing program entitled Advanced Technology Composite Aircraft Structure (ATCAS) is focused on t...