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Advanced structures technology applied to a supersonic cruise arrow-wing configuration
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Davis, G. W. Sakata, I. F. |
| Copyright Year | 1976 |
| Description | The application of advanced technology to a promising aerodynamic configuration was explored to investigate the improved payload range characteristics over the configuration postulated during the National SST Program. The results of an analytical study performed to determine the best structural approach for design of a Mach number 2.7 arrow-wing supersonic cruise aircraft are highlighted. The data conducted under the auspices of the Structures Directorate of the National Aeronautics and Space Administration, Langley Research Center, established firm technical bases from which further trend studies were conducted to quantitatively assess the benefits and feasibility of using advanced structures technology to arrive at a viable advanced supersonic cruise aircraft. |
| File Size | 2369996 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770011083 |
| Archival Resource Key | ark:/13960/t09w57d0q |
| Language | English |
| Publisher Date | 1976-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Structural Design Arrow Wings Supersonic Aircraft Aerodynamic Configurations Technology Assessment Feasibility Analysis Aircraft Configurations Mach Number Payloads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
