Loading...
Please wait, while we are loading the content...
Similar Documents
Subsonic longitudinal and lateral-directional static aerodynamic characteristics of a general research fighter configuration employing a jet sheet vortex generator
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ziegler, H. Huffman, J. K. Fox Jr., C. H. |
| Copyright Year | 1978 |
| Description | A configuration concept for developing vortex lift, which replaces the physical wing strake with a jet sheet generated fluid strake, was investigated on a general research fighter model. The vertical and horizontal location of the jet sheet with respect to the wing leading edge was studied over a momentum coefficient range from 0 to 0.24 in the Langley 7- by 10-foot high speed tunnel over a Mach number range from 0.3 to 0.8. The angle of attack range studied was from -2 to 30 deg at sideslip angles of 0, -5, and 5 deg. Test data are presented without analysis. |
| File Size | 16620893 |
| Page Count | 189 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780012128 |
| Archival Resource Key | ark:/13960/t7gr1q974 |
| Language | English |
| Publisher Date | 1978-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Vortex Sheets Static Aerodynamic Characteristics Stabilizers Fluid Dynamics Research Aircraft Subsonic Flow Wind Tunnel Tests Body-wing and Tail Configurations Vortex Generators Lateral Stability Fighter Aircraft Longitudinal Stability Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
