Loading...
Please wait, while we are loading the content...
Similar Documents
Free-Flight Investigation at Transonic and Supersonic Speeds of a Wing-Aileron Configuration Simulating the D-558-2 Airplane
| Content Provider | University of North Texas |
|---|---|
| Author | Sandahl, Carl A. |
| Organization | Langley Aeronautical Laboratory |
| Description | "An investigation of the rolling effectiveness at transonic and supersonic speeds of a wing-aileron configuration simulating the D-558-2 airplane has been made by means of a rocket-propelled test vehicle. The variation of rolling effectiveness with Mach number is similar to that obtained previously for tapered sweptback wings having full-span, 0.2-chord ailerons" (p. 1). |
| File Format | |
| Archival Resource Key | ark:/67531/metadc57666 |
| Language | English |
| Publisher Date | 2019-01-10 |
| Access Restriction | Open |
| Subject Keyword | rolling effectiveness D-558-2 aircraft wings |
| Content Type | Text |
| Resource Type | Report |