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Arrow-wing supersonic cruise aircraft structural design concepts evaluation. volume 1: sections 1 through 6
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Davis, G. W. Sakata, I. F. |
| Copyright Year | 1975 |
| Description | The structural approach best suited for the design of a Mach 2.7 arrow-wing supersonic cruise aircraft was investigated. Results, procedures, and principal justification of results are presented. Detailed substantiation data are given. In general, each major analysis is presented sequentially in separate sections to provide continuity in the flow of the design concepts analysis effort. In addition to the design concepts evaluation and the detailed engineering design analyses, supporting tasks encompassing: (1) the controls system development; (2) the propulsion-airframe integration study; and (3) the advanced technology assessment are presented. |
| File Size | 15501491 |
| Page Count | 566 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760021131 |
| Archival Resource Key | ark:/13960/t73v4bz2f |
| Language | English |
| Publisher Date | 1975-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Arrow Wings Supersonic Aircraft Airframes Technology Assessment Structural Design Criteria Aircraft Design Design Analysis Propulsion System Configurations Aircraft Control 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 |
