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Study of the feasibility aspects of flight testing an aeroelastically tailored forward swept research wing on a bqm-34f drone vehicle
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mourey, D. J. |
| Copyright Year | 1979 |
| Description | The aspects of flight testing an aeroelastically tailored forward swept research wing on a BQM-34F drone vehicle are examined. The geometry of a forward swept wing, which is incorporated into the BQM-34F to maintain satisfactory flight performance, stability, and control is defined. A preliminary design of the aeroelastically tailored forward swept wing is presented. |
| File Size | 15750006 |
| Page Count | 441 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800001956 |
| Archival Resource Key | ark:/13960/t3jx35w0r |
| Language | English |
| Publisher Date | 1979-09-03 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Flight Tests Stress Analysis Drone Aircraft Swept Forward Wings Structural Design Criteria Aeroelasticity Wing Loading Computer Aided Design 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 |
