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Theoretical prediction of the effects of vortex flows on the loading, forces, and moments of slender aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Spahr, J. R. |
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 1961 |
| Abstract | Effect of vortex flow on aerodynamic load, force, and stability of slender body aircraft |
| File Size | 1790394 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_19630004996 |
| Archival Resource Key | ark:/13960/t5h99sz7s |
| Language | English |
| Publisher Date | 1961-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamic Forces Aerodynamic Force Aerodynamic Load Aerodynamic Stability Aircraft Slender Body Vortex Flow Aerodynamic Loads Loading Moments Loads (forces) Slender Bodies Stability Vortices Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |