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Arrow-wing supersonic cruise aircraft structural design concepts evaluation. volume 3: sections 12 through 14
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Davis, G. W. Sakata, I. F. |
| Copyright Year | 1975 |
| Description | The design of an economically viable supersonic cruise aircraft requires the lowest attainable structural-mass fraction commensurate with the selected near-term structural material technology. To achieve this goal of minimum structural-mass fraction, various combinations of promising wing and fuselage primary structure were analyzed for the load-temperature environment applicable to the arrow wing configuration. This analysis was conducted in accordance with the design criteria specified and included extensive use of computer-aided analytical methods to screen the candidate concepts and select the most promising concepts for the in-depth structural analysis. |
| File Size | 17207457 |
| Page Count | 429 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760021133 |
| Archival Resource Key | ark:/13960/t1xd5p58v |
| Language | English |
| Publisher Date | 1975-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Arrow Wings Supersonic Aircraft Structural Design Criteria Fuselages Aircraft Design Design Analysis Aircraft Structures Thermal Stresses Computer Aided Design Loads Forces 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 |
