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Integration of a mechanical forebody vortex control system into the f-15
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Citurs, Kevin D. Ely, Wayne L. Harbaugh, Stephen P. Phillips, Ronald L. Hollingsworth, William B. Boalbey, Richard E. |
| Copyright Year | 1994 |
| Description | The goal of the F-15 Forebody Vortex Control (FVC) program is to develop a production FVC system for the F-15. The system may consist of either a mechanically actuated device such as the strakes developed for the HARV program, or a pneumatic device such as the port blowing system being tested on the X-29. Both types of systems are being evaluated under this program. Background information on the F-15 and a description and overview of forebody vortex controls (FVC) will be presented. |
| File Size | 615032 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19950007844 |
| Archival Resource Key | ark:/13960/t5m954w21 |
| Language | English |
| Publisher Date | 1994-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics X-29 Aircraft Strakes Vortices Wind Tunnel Tests Controllability Angle of Attack F-15 Aircraft Forebodies Blowers Pneumatics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
