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Investigation of the aerodynamic characteristics of a supersonic horizontal- attitude vtol airplane model at mach numbers of 1.57, 2.14, 2.54, and 2.87
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Franklin, A. E. Lust, R. M. |
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 1960 |
| Abstract | Drag and static longitudinal and lateral stability characteristics of supersonic horizontal attitude VTOL aircraft model in wind tunnel |
| File Size | 37197632 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_19670022403 |
| Archival Resource Key | ark:/13960/t4hm5xr0p |
| Language | English |
| Publisher Date | 1960-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamic Characteristics Supersonic Aircraft Vertical Takeoff Aircraft Wind Tunnel Models Aircraft Model Lateral Stability Longitudinal Stability Static Aerodynamic Characteristics Vtol Aircraft Aircraft Models Attitude (inclination) Drag Mach Number Static Stability Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |