Loading...
Please wait, while we are loading the content...
Similar Documents
Study for the optimization of a transport aircraft wing for maximum fuel efficiency. volume 1: methodology, criteria, aeroelastic model definition and results
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sweers, J. Linner, L. Conner, F. Radovcich, N. A. Dreim, D. Richardson, D. Okeefe, D. A. Pathak, S. K. Reaser, J. S. |
| Copyright Year | 1985 |
| Description | Work performed in the design of a transport aircraft wing for maximum fuel efficiency is documented with emphasis on design criteria, design methodology, and three design configurations. The design database includes complete finite element model description, sizing data, geometry data, loads data, and inertial data. A design process which satisfies the economics and practical aspects of a real design is illustrated. The cooperative study relationship between the contractor and NASA during the course of the contract is also discussed. |
| File Size | 13684304 |
| Page Count | 358 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850014067 |
| Archival Resource Key | ark:/13960/t94798h0c |
| Language | English |
| Publisher Date | 1985-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Finite Element Method Structural Weight Wings Transport Aircraft Structural Design Criteria Aircraft Design Nastran Aeroelasticity Computer Aided Design Operating Systems Computers Data Bases Structural Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
